Table Of Content

INDEX TO VOLUME 111 THE AERONAUTICAL JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY Volume CXl January-December 2007 Subject Index AERODYNAMICS AIR TRAFFIC MANAGEMENT A message from the editor. P. Bearman, November pp iv. Reducing environmental impacts of aviation with innovative air traffic A PIV investigation of the characteristics of micro-scale synthetic jets. management technologies. V. Williams, R.B. Noland, A. F. Guo and S. Zhong, pp 509-518. Majumdar, R. Toumi, W. Ochieng and J. Molloy, pp 741-749. Computational and experimental investigations of low-Reynolds- number flows past an aerofoil. W. Yuan, M. Khalid, J. Windte, U. AIRCRAFT DESIGN Scholz and R. Radespiel, pp 17-29. A review of supersonic businesjse t design issues. H. Smith, pp 761- Effect of plunging amplitude on the performance of a wind turbine 776. blade section. M.R. Soltani and F. Rasi Marzabadi, pp 571-587. Flow control with active dimples. S. Dearing, S. Lambert and J. AIRWORTHINESS Morrison, pp 705-714. A proposed reference framework for unmanned aerial vehicle and High performance computing and computational aerodynamics in the system airworthiness requirements. A. Maneschijn, T. Jones, T.W. UK. D.R. Emerson, A.J. Sunderland, M. Ashworth and K._J. von Backstrém and L.A. Ingham, pp 345-358. Badcock, pp 125-131. Investigation on the aerodynamic performance on an ejection seat. BOOK REVIEWS — BY AUTHOR D.H. Chen, W.H. Wu, J.J. Wang and Y. Huang, pp 373-380. Aliabadi, M.H. and Guagliano, M. Fractures and Damage of Large-eddy simulation of separated flow over a swept wing with Composites, p 826. approximate near-wall modelling. N. Li and M.A. Leschziner, pp Anderson, J.D. Hypersonic and High Temperature Gas Dynamics, 689-697. Second Edition, p 121. Large-eddy simulation of twin impinging jets in cross-flow. Q. Li, Armstrong, K.B. et a/ Care and Repair of Advanced Composites, G.J. Page and J.J. McGuirk, pp 195-206. Second Edition, p 120. Parallel adjoint-based optimisation of a blended wing body aircraft Borgnakke, C. and Sonntag, R.E. Introduction to Engineering with shock control bumps. W.S. Wong, A. Le Moigne and N. Qin, Thermodynamics, Second Edition, p 122. pp 165-174. Cloud, M.J. and Moore, R.E. Computational Functional Aanlysis, Prediction of aerodynamic forces on a helicopter fuselage. A. Second Edition, p 603. Filippone, pp 175-184. Curtis, P., Kuhn, R.F.E. and Margason, R.J. Jet Induced Effects: the Prediction of drag and lift of wings from velocity and vorticity fields. Aerodynamics of Jet and Fan Powered V/STOL Aircraft in Hover G. Zhu, P.W. Bearman and J.M.R. Graham, pp 699-704. and Transition, p 670. Remarks on the nonlinear dynamics of a typical aerofoil section in Dodson, B. and Schwab, H. Accelerated Testing; a Practioner’s Guide dynamic stall. U. Galvanetto, J. Peiro and C. Chantharasenawong, to Accelerated and Reliability Testing, p 119. pp 731-739. Dowell, E.H. (Ed) et al A Modern Course in Aeroelasticity, Fourth The onset of compressibility effects for aerofoils in ground effect. Edition, p 120. Technical note, G. Doig, T.J. Barber, E. Leonardi and A.J. Neely, Dreier, M.E. Introduction to Helicopter and Tiltrotor Flight pp 797-806. Simulation, p 405. Fillippone, A. Flight Performance of Fixed and Rotary Wing Aircraft, AEROSPACE ENGINEERING p 603. New commercial opportunities in space. D.M. Ashford, pp 61-75. Fisher, L.W. Selection of Engineering Materials and Adhesives, p On different parameterisation methods to analyse spacecraft attitude 471. manoeuvres in the presence of attitude constrainsts. G. Radice and Flack, J.D. Fundamentals uf Jet Propulsion with Applications, p 470. M. Casasco, pp 335-342. Fleeman, E.L. Tactical Missile Design, Second Edition, p 119. Performance characterisation of MPD thrusters. T.R. Nada, Guagliano, M. and Aliabadi, M.H. Fractures and Damage of pp 443. Composites, p 826. 816 THE AERONAUTICAL JOURNAL DECEMBER 2007 Henderson, D.M. Applied Cartesian Tensors for Aerospace Tischler, M.B. and Remple, R.K. Aircraft and Rotorcraft System Simulators, p 121. Identification: Engineering Methods with Flight Test Examples, p 601. Howe, M.S. Hydrodynamics and Sound, p 668. Ugaral, A.C. Mechanics of Materials, p 740. Jategaonkar, R.V. Flight Vehicle System Identification: a Time Wagg, D. (Ed) et al. Adaptive Structures: Engineering Applications, p Domain Methodology. Progess in Aeronautics and Astronautics 827. series Vol 216, p 601. Wiley, R.G. ELINT: the Interception and Analysis of Radar Signals, p Kiusalaas, J. Numerical Methods in Engineering with MATLAB, p 280. 280. Kiusalaas, J. Numerical Methods in Engineering with Python, p 280. Zarchan, P. Tactical and Strategic Missile Guidance, Fifth Edition, Klein, V. and Morelli, E.A. Aircraft System Identification: Theory and Progress in Aeronautics and Astronautics series Vol 219, p 406, Practice, p 602. 470. Knight, D.D. Elements of Numerical Methods for Compressibility Flows, p 740. BOOK REVIEWS — BY TITLE Kraige, L.G. and Meriam, J.L. Engineering Mechanics (Vol 2) — A Modern Course in Aeroelasticity, Fourth Edition, E.H. Dowell (Ed) Dynamics, Sixth Edition, p 406. etal, p 120. Krysinski, T. and Malburet, F. Mechanical Vibrations: Active and Adaptive Structures: Engineering Applications, D. Wagg (Ed) et al, p Passive Control, p 668 827. Kuhn, R.F.E., Margason, R.J. and Curtis, P. Jet Induced Effects: the Accelerated Testing; a Practioner’s Guide to Accelerated and Aerodynamics of Jet and Fan Powered V/STOL Aircraft in Hover Reliability Testing, B. Dodson and H. Schwab, p 119. and Transition, p 670. Advanced Vector Analysis for Scientists and Engineers, M. Rahman, Kutz, M. (Ed) Environmentally Conscious Mechanical Design, p 669. p 668. Kutz, M. (Ed) Environmentally Conscious Manufacturing, p 670. Aircraft and Rotorcraft System Identification: Engineering Methods Leishmann, J.G. Principles of Helicopter Aerodynamics, Second with Flight Test Examples, M.B. Tischler and R.K. Remple, p 601. edition, p 825. Aircraft Design — a Conceptual Approach, Fourth Edition, D.P. Levin, E.M. Dynamic Analysis of Space Tether Missions. American Raymer, p 120. Astronautical Society (AAS) Advances in the Astronautical Aircraft Performance, M. Saarlas, p 669. Sciences series Vol 126, p 750. Aircraft System Identification: Theory and Practice, V. Klein and E.A. Lorenz, R.D. Spinning Flight: Dynamics of Frisbees, Boomerangs, Morelli, p 602. Samaras and Skipping Stones, p 122. Applied Cartesian Tensors for Aerospace Simulators, D.M. Malburet, F. and Krysinski, T. Mechanical Vibrations: Active and Henderson, p 121. Passive Control, p 668. Care and Repair of Advanced Composites, Second Edition, K.B. Margason, R.J., Curtis, P. and Kuhn, R.F.E. Jet Induced Effects: the Armstrong et al, p 120. Aerodynamics of Jet and Fan Powered V/STOL Aircraft in Hover Computational Functional Analysis, Second Edition, R.E. Moore and and Transition, p 670. M.J. Cloud, p 603. Mattingly, J.D. Elements of Propulsion: Gas Turbines and Rockets, Dynamic Analysis of Space Tether Missions. American Astronautical Second Edition, p 119. Society (AAS) Advances in the Astronautical Sciences series Vol Meriam, J.L. and Kraige, L.G. Engineering Mechanics (Vol 2) — 126, E.M. Levin, p 750. Dynamics, Sixth Edition, p 406. Elements of Numerical Methods for Compressibility Flows, D.D. Moore, R.E. and Cloud, M.J. Compuiational Functional Aanlysis, Knight, p 740. Second Edition, p 603. Elements of Propulsion: Gas Turbines and Rockets, Second Edition, Moran, M.J. and Shapiro, H.N. Fundamentals of Engineering J.D. Mattingly, p 119. Thermodynamics, Fifth Edition, p 122. ELINT: the Interception and Analysis of Radar Signals, R.G. Wiley, p Morelli, E.A. and Klein, V. Aircraft System Identification: Theory and 280. Practice, p 602. Engineering Mechanics (Vol 2) — Dynamics, Sixth Edition, J.L. Mueller, T.J. et al Introduction to the Design of Fixed-Wing Micro Meriam and L.G. Kraige, p 406. Air Vehicles: including Three Case Studies, p 405. Environmentally Conscious Manufacturing, M. Kutz (Ed), p 670. Pai, P.F. Highly Flexible Structures: Modeling, Computation and Environmentally Conscious Mechanical Design, M. Kutz (Ed), p 669. Experimentation, p 826. Flight Performance of Fixed and Rotary Wing Aircraft, A. Fillippone, Rahman, M. Advanced Vector Analysis for Scientists and Engineers, p 603. p 668. Flight Vehicle System Identification: a Time Domain Methodology. Raymer, D.P. Aircraft Design - a Conceptual Approach, Fourth Progess in Aeronautics and Astronautics series Vol 216, R.V. Edition, p 120. Jategaonkar, p 601. Raymer, D.P. RDS-Student: Sofrtware for Aircraft Design, Sizing and Fractures and Damage of Composites. M. Guagliano and M.H Performance, p 120. Aliabadi, p 826. Remple, R.K. and Tischler, M.B. Aircraft and Rotorcraft System Fundamentals of Engineering Thermodynamics, Fifth Edition, M.J. Identification: Engineering Methods with Flight Test Examples, p Moran and H.N. Shapiro, p 122. 601. Fundamentals of Jet Propulsion with Applications, J.D. Flack, p 470. Saarlas, M. Aircraft Performance, p 669. Health Monitoring of Aerospace Structures: Smart Sensor Schwab, H. and Dodson, B. Accelerated Testing; a Practioner’s Guide Technologies and Signal Processing, W. Staszewski et al, p 750. to Accelerated and Reliability Testing, p 119. Highly Flexible Structures: Modeling, Computation and Shapiro, H.N. and Moran, M.J. Fundamentals of Engineering Experimentation. P.F. Pai, p 826. Thermodynamics, Fifth Edition, p 122. Hydrodynamics and Sound, M.S. Howe, p 668. Sonntag, R.E. and Borgnakke, C. Introduction to Engineering Hypersonic and High Temperature Gas Dynamics, Second Edition, Thermodynamics, Second Edition, p 122. J.D. Anderson, p 121. Staszewski, W. ef al Health Monitoring of Aerospace Structures: Introduction to Engineering Thermodynamics, Second Edition, R.E. Smart Sensor Technologies and Signal Processing, p 750. Sonntag and C. Borgnakke, p 122. INDEX TO VOLUME 111 Introduction to Helicopter and Tiltrotor Flight Simulation, M.E. Large-eddy simulation of separated flow over a swept wing with Dreier, p 405. approximate near-wall modelling. N. Li and M.A. Leschziner, pp Introduction to the Design of Fixed-Wing Micro Air Vehicles: 689-697. including Three Case Studies, T.J. Mueller ef al, p 405. Numerical study of transonic cavity flows using large-eddy and Jet Induced Effects: the Aerodynamics of Jet and Fan Powered detached-eddy simulation. P. Nayyar, G.N. Barakos and K.J. V/STOL Aircraft in Hover and Transition, R.F.E. Kuhn, R.J. Badcock, pp 153-164. Margason and P. Curtis, p 670. Parallel adjoint-based optimisation of ab lended wing body aircraft Mechanical Vibrations: Active and Passive Control, T. Krysinski and with shock control bumps. W.S. Wong, A. Le Moigne and N. Qin, F. Malburet, p 668. pp 165-174. Mechanics of Materials, A.C. Ugaral, p 740. The representation ofG T component maps using Mach numbers. V.E. Numerical Methods in Engineering with MATLAB, J. Kiusalaas, p Kyritsis, P. Pilidis and K. Ramsden, pp 453-460. 280. Three-dimensional indicial response of finite aspect ratio yawed Numerical Methods in Engineering with Python, J. Kiusalaas, p 280. wings. C.E. Manglano-Villamarin and S.T. Shaw, pp 359-371. Principles of Helicopter Aerodynamics, Second edition. J.G. Towards a full two dimensional gas turbine performance simulator. V. Leishmann, p 825. Pachidis, P. Pilidis, L. Marinai and I. Templalexis, pp 433-442. RDS-Student: Sofrtware for Aircraft Design, Sizing and Performance, D.P. Raymer, p 120. DESIGN Selection of Engineering Materials and Adhesives, L.W. Fisher, p Design of fixed wing micro air vehicles. P. Cosyn, pp 315-326. 471. On the benefits of lower Mach number aircraft cruise. A. Filippone, Spinning Flight: Dynamics of Frisbees, Boomerangs, Samaras and pp 531-542. Skipping Stones, R.D. Lorenz, p 122. Tactical and Strategic Missile Guidance, Fifth Edition, Progress in ENVIRONMENTAL ENGINEERING Aeronautics and Astronautics series Vol 219, P. Zarchan, p 406, Lean engineering: a framework for doing the right thing right. H.L. 470. McManus, A. Haggerty and E. Murman, pp 105-114. Tactical Missile Design, Second Edition, E.L. Fleeman, p 119, A change in the calculated impact of supersonic aircraft NOx emissions on the atmosphere. O. Dessens, H.L. Rogers and J.A. COMPOSITES Pyle, pp 311-314. A study of secondary instabilities in postbuckling composite ‘Greener’ civil aviation using air-to-air refuelling — relating aircraft aerostructures. B.G. Falzon and M. Cerini, pp 715-729. design efficiency and tanker offload efficiency. R.K. Nangia, pp Analysis of composite plates with variable stiffness using Galerkin 589-592. Method. E. Senocak and H. Tanriover, pp 247-255. On the benefits of lower Mach number aircraft cruise. A. Filippone, pp 531-542. COMPUTATIONAL FLUID DYNAMICS Reducing environmental impacts of aviation with innovative air traffic Achieving high parallel performance for an unstructured unsteady management technologies. V. Williams, R.B. Noland, A. turbomachinery CFD code. N. Hills, pp 185-193. Majumdar, R. Toumi, W. Ochieng and J. Molloy, pp 741-749. An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion control analysis. A.M. Savill, G.A. Richardson and W.N. FLIGHT CONTROL DYNAMICS Dawes, pp 133-144. Aircraft flight characteristics in conditions of windshear and icing. Y. Application of a parallel rotor CFD code on HPCx. C.B. Allen, A.G. Cao and K. Yuan, pp 41-49. Sunderland and R. Johnstone, pp 145-152. Dynamic gain scheduled control of aH awk scale model. T. Computational and experimental investigations of low-Reynolds- Richardson, M. Lowenberg, C. Jones and A. Dubs, pp 461-469. number flows past an aerofoil. W. Yuan, M. Khalid, J. Windte, U. Estimation of lateral-directional parameters using neural networks based Scholz, and R. Radespiel, pp 17-29. modified delta method. S. Singh and A. K. Ghosh, pp 659-667. High performance computing and computational aerodynamics in the Relationships between flying qualities and flight tests parameters for UK. D.R. Emerson, A.J. Sunderland, M. Ashworth and K.J. the F/A-18 aircraft. R.M. Botez and M. Rotaru, pp 281-282. Badcock, pp 125-131. Some analytical and numerical solutions for the safe turn manoeuvres The onset of compressibility effects for aerofoils in ground effect. of agricultural aircraft — an overview. B. Rasuo, pp 593-599. Technical note, G. Doig, T.J. Barber, E. Leonardi and A.J. Neely, pp 797-806. FLIGHT SIMULATION Addressing pose estimation issues for machine vision based UAV COMPUTATIONAL TECHNIQUES autonomous aerial refuelling. G,C ampa, M.R. Napolitano and M. A static compressible flow model of synthetijce t actuators. H. Tang Perhinschi, pp 389-396. and S. Zhong, pp 421-431. Aircraft cost modelling using the genetic causal technique within a FLIGHT TEST systems engineering approach. R. Curran, S. Castagne, J. Early, Relationships between flying qualities and flight tests parameters for M. Price, S. Raghunathan, J. Butterfield and A. Gibson, pp 409- the F/A-18 aircraft. R.M. Botez and M. Rotaru, pp 281-282. 420. Experimental and computational study of unsteady hypersonic cavity HISTORY flows. S. Creighton and R. Hillier, pp 673-688. The Victoria University of Manchester’s contributions to the Flight data reduction methodology for performance evaluation and development of aeronautics. J.A.D. Ackroyd, pp 473-493. comparison of model-following adaptive control laws. M.G. Perhinschi and M.R. Napolitano, pp 807-814. INDUSTRY High resolution computational unsteady aerodynamic techniques Strategic Destruction of the Western commercial aircraft sector: applied to maneouvering UCAVs. S.A. Morton, R.M. Cummings, implications of system integration and international risk-sharing J.R. Forsythe and K. Wurtzler, pp 397-404. business models. D. Pritchard and A. MacPherson, pp 327-334. 818 THE AERONAUTICAL JOURNAL DECEMBER 2007 JETS STRUCTURES A PIV investigation of the characteristics of micro-scale synthetic jets. A study of secondary instabilities in postbuckling composite F. Guo and S. Zhong, pp 509-518. aerostructures. B.G. Falzon and M. Cerini, pp 715-729. A static compressible flow model of synthetic jet actuators. H. Tang Analysis of composite plates with variable stiffness using Galerkin and S. Zhong, pp 421-431. Method. E. Senocak and H. Tanriover, pp 247-255. Application of synthetic jet actuators for the modification of the Development of a parametric-based indirect aircraft structural usage characteristics of separated shear layers on slender wings. M. monitoring system using artificial neural networks. S.C. Reed, pp Watson, A.J. Jaworski and N.J. Wood, pp 519-529. 209-230. Large-eddy simulation of twin impinging jets in cross-flow. Q. Li, Three dimensional tensile stress concentration in countersunk. A. G.J. Page and J.J. McGuirk, pp 195-206. Bhargava and K. N. Shivakumar, pp 777-786. LIGHTER THAN AIR SYSTEMS Performance of non-rigid airships operating in the neutral buoyancy An optimal-fuzzy two-phase CLOS guidance law design using ant condition. G.E. Dorrington, pp 89-103. colony optimisation. H. Nobahari and S.H. Pourtakdoust, pp 621- 636. PROPULSION Development of a parametric-based indirect aircraft structural usage A numerical study of high pressure turbine forced response in the monitoring system using artificial neural networks. S.C. Reed, pp presence of damaged nozzle guide vanes. L. di Mare, M. Imregun, 209-230. A.D. Smith and R. Elliott, pp 751-757. Developments in RF simulator technology — approaching the Achieving high parallel performance for an unstructured unsteady affordable limit. M. Pywell, pp 545-560. turbomachinery CFD code. N. Hills, pp 185-193. Measuring the effect of helicopter rotors on GPS reception. G.J. An idea ofd istributed parameter control for scramjet engines. Y. Brodin, J.A. Cooper and J.R.A. Stevens, pp 561-570. Daren, C. Tao and B. Wen, pp 787-796. An unsteady, moving mesh CFD simulation for Harrier hot-gas The MIL-STD-1553B data bus: What does the future hold? D.R. ingestion control analysis. A.M. Savill, G.A. Richardson and W.N. Bracknell, pp 231-246. Dawes, pp 133-144. Use of Global Positioning System velocity outputs for determining Effect of stagnation temperature on supersonic flow parameters airspeed measurement error. G.B. Gratton, pp 381-388. application for air in nozzles. T. Zebbiche and Z. Youbi, pp 31-40. Loss reduction on ultra high lift low-pressure turbine blades using TESTING FACILITIES AND TECHNOLOGIES selective roughness and wake unsteadiness. R.J. Howell and K.M. A review of some current research on pressure sensitive paint and Roman, pp 257-206. thermographic phosphor techniques. K. Kontis, pp 495-508. Methods for the design of energy efficient high-speed aerospace vehicles. Design and performance of thin, circular arc, wind-tunnel turning D. Riggins, T.Taylor, L. Terhune and D. Moorhouse, pp 297-309. vanes. G. Johl, M. Passmore and P. Render, pp 115-118. Numerical exploration of starting process in supersonic nozzle. S. Developments in RF simulator technology — approaching the Saha and D. Chakraborty, pp 51-58. affordable limit. M. Pywell, pp 545-560. Performance characterisation of MPD thrusters. T.R. Nada, pp 443-452. Experimental and computational study of unsteady hypersonic cavity Scramjets. M. Smart, pp 605-619. flows. S. Creighton and R. Hillier, pp 673-688. The representation of GT component maps using Mach numbers. V.E. Optical imaging techniques for hypersonic impulse facilities. T.J. ‘Kyritsis, P. Pilidis and K. Ramsden, pp 453-460. McIntyre, H. Kleine and A.F.P. Houwing, pp 1-16. Towards a full two dimensional gas turbine performance simulator. V. Pachidis, P. Pilidis, L. Marinai and I. Templalexis, pp 433-442. TRAINING A systems approach to training aeronautical decision making: from ROTORCRAFT identifying training needs to verifying training solutions. D. Harris Modelling and vibration ofa non-classical tilt-rotor wing system. O. and W.-C. Li, pp 267-279. Song, H.D. Kwon and L. Librescu, pp 285-295. Application of a parallel rotor CFD code on HPCx. C.B. Allen, A.G. UNMANNED AIR VEHICLES Sunderland and R. Johnstone, pp 145-152. A proposed reference framework for unmanned aerial vehicle and Measuring the effect of helicopter rotors on GPS reception. G.J. system airworthiness requirements. A. Maneschijn, T. Jones, T.W. Brodin, J.A. Cooper and J.R.A. Stevens, pp 561-570. von Backstrém and L.A. Ingham, pp 335-342. Modelling the interaction of helicopter main rotor and tail rotor wakes. Addressing pose estimation issues for machine vision based UAV T.M. Fletcher and R.E. Brown, pp 637-643. autonomous aerial refuelling. G,C ampa, M.R. Napolitano and M. Prediction of aerodynamic forces on a helicopter fuselage. A. Filippone, pp 175-184. Perhinschi, pp 389-396. Rotorcraft simulation modelling and validation for control law design. Design of fixed wing micro air vehicles. P. Cosyn, pp 315-326. B.J. Manimala, D.J. Walker, G.D. Padfield, M. Voskuijl and A.W. High resolution computational unsteady aerodynamic techniques Gubbels, pp 77-88. applied to maneouvering UCAVs. S.A. Morton, R.M. Cummings, Survivability of helicopter with individual blade primary control failure. J.R. Forsythe and K. Wurtzler, pp 397-404. R. Ganguli, B. Jehnert, J. Wolfram and P. Voersmann, pp 645-657. VIBRATION SIMULATION Modelling and vibration of a non-classical tilt-rotor wing system. O. Aircraft flight characteristics in conditions of windshear and icing. Y. Song, H.D. Kwon and L. Librescu, pp 285-295. Cao and K. Yuan, pp 41-49. Rotorcraft simulation modelling and validation for control law design. WAKES B.J. Manimala, D.J. Walker, G.D. Padfield, M. Voskuijl and A.W. Modelling the interaction of helicopter main rotor and tail rotor wakes. Gubbels, pp 77-88. T.M. Fletcher and R.E. Brown, pp 637-643. INDEX TO VOLUME 111 Author Index ACKROYD, J.A.D. CASTAGNE, S., EARLY, J., PRICE, M., RAGHUNATHAN, S., The Victoria University of Manchester’s contributions to the development BUTTERFIELD, J., GIBSON, A. and CURRAN, R. of aeronautics, pp 473-493. Aircraft cost modelling using the genetic causal technique within a systems engineering approach, pp 409-420. ALLEN, C.B., SUNDERLAND, A.G. and JOHNSTONE, R. Application of a parallel rotor CFD code on HPCx, pp 145-152. CERINI, M. and FALZON, B.G. A study of secondary instabilities in postbuckling composite ASHFORD, D.M. aerostructures, pp 715-729. New commercial opportunities in space, pp 61-75. CHAKRABORTY, D. and SAHA, S. ASHWORTH, M. and BADCOCK, K.J., EMERSON, D.R. and Numerical exploration of starting process in supersonic nozzle, pp 51-58. SUNDERLAND, A.J. High performance computing and computational aerodynamics in the UK, CHANTHARASENAWONG, C., GALVANETTO, U. and PEIRO, J. pp 125-131. Remarks on the nonlinear dynamics of a typical aerofoil section in dynamic stall, pp 731-739. BADCOCK, K.J., EMERSON, D.R., SUNDERLAND, A.J. and ASHWORTH, M. CHEN, D.H., WU, W.H., WANG, J.J. and HUANG, Y. High performance computing and computational aerodynamics in the UK, Investigation on the aerodynamic performance on an ejection seat, pp 373-380. pp 125-131. COOPER, J.A., STEVENS, J.R.A. and RRODIN, G.J. BADCOCK, K.J., NAYYAR, P. and BARAKOS, G.N. Measuring the effect of helicopter rotors on GPS reception, pp 561-570. Numerical study of transonic cavity flows using large-eddy and detached- eddy simulation, pp 153-164. COSYN, P. Design of fixed wing micro air vehicles, pp 315-326. BARAKOS, G.N., BADCOCK, K.J. and NAYYAR, P. Numerical study of transonic cavity flows using large-eddy and detached- CREIGHTON, S. and HILLIER, R. eddy simulation, pp 153-164. Experimental and computational study of unsteady hypersonic cavity flows, pp 673-688. BARBER, T.J., LEONARDI, E., NEELY, A.J. and DOIG, G. The onset of compressibility effects for aerofoils in ground effect, Technical CUMMINGS, R.M., FORSYTHE, J.R., WURTZLER, K. and note, pp 797-806. MORTON, S.A. High resolution computational unsteady aerodynamic techniques applied BEARMAN, P.W. to maneouvering UCAVs, pp 397-404. A message from the editor, November pp iv. CURRAN, R., CASTAGNE, S., EARLY, J., PRICE, M., BEARMAN, P.W., GRAHAM, J.M.R. and ZHU, G. RAGHUNATHAN, S., BUTTERFIELD, J. and GIBSON, A. Prediction of drag and lift of wings from velocity and vorticity fields, pp Aircraft cost modelling using the genetic causal technique w ithin a 699-704. systems engineering approach, pp 409-420. BHARGAVA, A. and SHIVAKUMAR, K.N. DAREN, Y., WEN, B. and TAO, C. Three dimensional tensile stress concentration in countersunk, pp 777-786. An idea of distributed parameter control for scramjet engines, pp 787-796 BOTEZ, R.M. and ROTARU, M. DEARING, S., LAMBERT, S. and MORRISON, J. Relationships between flying qualities and flight tests parameters for the Flow control with active dimples, pp 705-714. F/A-18 aircraft, pp 281-282. DESSENS, O., ROGERS, H.L. and PYLE, J.A. BRACKNELL, D.R. A change in the calculated impact of supersonic aircraft NOx emissions on The MIL-STD-1553B data bus: What does the future hold?, pp 231-246. the atmosphere, pp 311-314. BRODIN, G.J., COOPER, J.A. and STEVENS, J.R.A. DI MARE, L., IMREGUN, M., SMITH, A.D. and ELLIOTT, R. Measuring the effect of helicopter rotors on GPS reception, pp 561-570. A numerical study of high pressure turbine forced response in the presence of damaged nozzle guide vanes, pp 751-757. BROWN, R.E. and FLETCHER, T.M. Modelling the interaction of helicopter main rotor and tail rotor wakes, pp DOIG, G., BARBER, T.J., LEONARDI, E. and NEELY, A.J. 637-643. The onset of compressibility effects for aerofoils in ground effect, Technical note, pp 797-806. BUTTERFIELD, J., GIBSON, A., CURRAN, R., CASTAGNE, S., EARLY, J., PRICE, M. and RAGHUNATHAN, S. DORRINGTON, G.E. Aircraft cost modelling using the genetic causal technique within a Performance of non-rigid airships operating in the neutral buoyancy systems engineering approach, pp 409-420. condition, pp 89-103. CAMPA, G., NAPOLITANO, M.R. and PERHINSCHI, M. DUBS, A., RICHARDSON, T., LOWENBERG, M. and JONES, C. Addressing pose estimation issues for machine vision based UAV Dynamic gain scheduled control of aH awk scale model, pp 461-469. autonomous aerial refuelling, pp 389-396. EARLY, J., PRICE, M., RAGHUNATHAN, S., BUTTERFIELD, J., CAO, Y. and YUAN, K. GIBSON, A., CURRAN, R. and CASTAGNE, S. Aircraft flight characteristics in conditions of windshear and icing, pp 41- Aircraft cost modelling using the genetic causal technique within a 49. systems engineering approach, pp 409-420. CASASCO, M. and RADICE, G. ELLIOTT, R., DI MARE, L., IMREGUN, M. and SMITH, A.D. On different parameterisation methods to analyse spacecraft attitude A numerical study of high pressure turbine forced response in the presence manoeuvres in the presence of attitude constrainsts, pp 335-342. of damaged nozzle guide vanes, pp 751-757. 820 THE AERONAUTICAL JOURNAL DECEMBER 2007 EMERSON, D.R., SUNDERLAND, A.J., ASHWORTH, M. and HUANG, Y., CHEN, D.H., WU, W.H. and WANG, J.J. BADCOCK, K.J. Investigation on the aerodynamic performance on an ejection seat, pp 373-380. High performance computing and computational aerodynamics in the UK, pp 125-131. IMREGUN, M., SMITH, A.D., ELLIOTT, R. and DI MARE, L. A numerical study of high pressure turbine forced response in the presence FALZON, B.G. and CERINI, M. of damaged nozzle guide vanes, pp 751-757. A study of secondary instabilities in postbuckling composite aerostructures, pp 715-729. INGHAM, L.A., MANESCHIJN, A., JONES, T. and VON BACKSTROM, T.W. FILIPPONE, A. A proposed reference framework for unmanned aerial vehicle and system Prediction of aerodynamic forces on a helicopter fuselage, pp 175-184. airworthiness requirements, pp 345-358. FILIPPONE, A. JAWORSKI, A.J., WOOD, N.J. and WATSON, M. On the benefits of lower Mach number aircraft cruise, pp 531-542. Application of synthetic jet actuators for the modification of the characteristics of separated shear layers on slender wings, pp 519-529. FLETCHER, T.M. and BROWN, R.E. Modelling the interaction of helicopter main rotor and tail rotor wakes, pp JEHNERT, B., WOLFRAM, J.,. VOERSMANN, P. and GANGULI, R. 637-643. Survivability of helicopter with individual blade primary control failure, pp 645-657. FORSYTHE, J.R., WURTZLER, K., MORTON, S.A. and CUMMINGS, R.M. JOHL, G., PASSMORE, M. and RENDER, P. High resolution computational unsteady aerodynamic techniques applied Design and performance oft hin, circular arc, wind-tunnel turning vanes, to maneouvering UCAVs, pp 397-404. pp 115-118. GALVANETTO, U., PEIRO, J. and CHANTHARASENAWONG, C. JOHNSTONE, R., ALLEN, C.B. and SUNDERLAND, A.G. Remarks on the nonlinear dynamics of a typical aerofoil section in Application of a parallel rotor CFD code on HPCx, pp 145-152. dynamic stall, pp 731-739. JONES, C., DUBS, A., RICHARDSON, T. and LOWENBERG, M. GANGULL, R., JEHNERT, B., WOLFRAM, J. and VOERSMANN, P. Dynamic gain scheduled control of aH awk scale model, pp 461-469. Survivability of helicopter with individual blade primary control failure, pp 645-657. JONES, T., VON BACKSTROM, T.W., INGHAM, L.A. and MANESCHIJN, A. s GHOSH, A.K. and SINGH, S. A proposed reference framework for unmanned aerial vehicle and system Estimation of lateral-directional parameters using neural networks based airworthiness requirements, pp 345-358. modified delta method, pp 659-667. KHALID, M., WINDTE, J., SCHOLZ, U., RADESPIEL, R. and YUAN, W. GIBSON, A., CURRAN, R., CASTAGNE, S., EARLY, J., PRICE, M., Computational and experimental investigations of low-Reynolds-number RAGHUNATHAN, S. and BUTTERFIELD, J. flows past an aerofoil, pp 17-29. Aircraft cost modelling using the genetic causal technique within a systems engineering approach, pp 409-420. KLEINE, H, HOUWING, A.F.P. and MCINTYRE, T.J., Optical imaging techniques for hypersonic impulse facilities, pp 1-16. GRAHAM, J.M.R., ZHU, G. and BEARMAN, P.W. Prediction of drag and lift of wings from velocity and vorticity fields, pp KONTIS, K. 699-704. A review of some current research on pressure sensitive paint and thermographic phosphor techniques, pp 495-508. GRATTON, G.B. Use of Global Positioning System velocity outputs for determining KWON, H.D., LIBRESCU, L. and SONG, O. airspeed measurement error, pp 381-388. Modelling and vibration of a non-classical tilt-rotor wing system, pp 285- 295. GUBBELS, A.W., MANIMALA, B.J., WALKER, D.J., PADFIELD, G.D. and VOSKUIJL, M. KYRITSIS, V.E., PILIDIS, P. and RAMSDEN, K. Rotorcraft simulation modelling and validation for control law design, pp 77-88. The representation ofG T component maps using Mach numbers, pp 453-460. GUO, F. and ZHONG, S. LAMBERT, S., MORRISON, J. and DEARING, S. A PIV investigation of the characteristics of micro-scale synthetic jets, pp Flow control with active dimples, pp 705-714. 509-518. LE MOIGNE, A., QIN, N. and WONG, W.S. HAGGERTY, A., MURMAN, E. and MCMANUS, H.L. Parallel adjoint-based optimisation of ab lended wing body aircraft with Lean engineering: a framework for doing the right thing right, pp 105-114. shock control bumps, pp 165-174. HARRIS, D. and LI, W.-C. LEONARDI, E., NEELY, A.J., DOIG, G. and BARBER, T.J. A systems approach to training aeronautical decision making: from The onset of compressibility effects for aerofoils in ground effect, Technical identifying training needs to verifying training solutions, pp 267-279. note, pp 797-806. HILLIER, R. and CREIGHTON, S. LESCHZINER, M.A. and LI, N. Experimental and computational study of unsteady hypersonic cavity Large-eddy simulation of separated flow over a swept wing with flows, pp 673-688. approximate near-wall modelling, pp 689-697. HILLS, N. LI, N. and LESCHZINER, M.A. Achieving high parallel performance for an unstructured unsteady Large-eddy simulation of separated flow over a swept wing with turbomachinery CFD code, pp 185-193. approximate near-wall modelling, pp 689-697. HOUWING, A.F.P., MCINTYRE, T.J. and KLEINE, H. LI, Q., PAGE, G.J. and MCGUIRK, J.J. Optical imaging techniques for hypersonic impulse facilities, pp 1-16. Large-eddy simulation of twin impinging jets in cross-flow, pp 195-206. HOWELL, R.J. and ROMAN, K.M. LI, W.-C. and HARRIS, D. Loss reduction on ultra high lift low-pressure turbine blades using A systems approach to training aeronautical decision making: from selective roughness and wake unsteadiness, pp 257-206. identifying training needs to verifying training solutions, pp 267-279. INDEX TO VOLUME 111 LIBRESCU, L., SONG, O. and KWON, H.D. NAYYAR, P., BARAKOS, G.N. and BADCOCK, K.J. Modelling and vibration of a non-classical tilt-rotor wing system, pp 285- Numerical study of transonic cavity flows using large-eddy and detached- 295. eddy simulation, pp 153-164. LOWENBERG, M., JONES, C., DUBS, A. and RICHARDSON, T. NEELY, A.J., DOIG, G., BARBER, T.J. and LEONARDI, E. Dynamic gain scheduled control of aH awk scale model, pp 461-469. The onset of compressibility effects for aerofoils in ground effect, Technical note, pp 797-806. MACPHERSON, A. and PRITCHARD, D. Strategic destruction of the Western commercial aircraft sector: NOBAHARI, H. and POURTAKDOUST, S.H. implications of system integration and international risk-sharing business An optimal-fuzzy two-phase CLOS guidance law design using ant colony models, pp 327-334. optimisation, pp 621-636. MAJUMDAR, A., TOUMI, R., OCHIENG, W., MOLLOY, J., NOLAND, R.B., MAJUMDAR, A., TOUMI, R., OCHIENG, W., WILLIAMS, V. and NOLAND, R.B. MOLLOY, J. and WILLIAMS, V. Reducing environmental! impacts of aviation with innovative air traffic Reducing environmental impacts of aviation with innovative air traffic management technologies, pp 741-749. management technologies, pp 741-749. MANESCHUJN, A., JONES, T., VON BACKSTROM, T.W. and OCHIENG, W., MOLLOY, J., WILLIAMS, V., NOLAND, R.B., INGHAM, L.A. MAJUMDAR, A. and TOUMIL, R. A proposed reference framework for unmanned aerial vehicle and system Reducing environmental impacts of aviation with innovative air traffic airworthiness requirements, pp 345-358. management technologies, pp 741-749. MANGLANO-VILLAMARIN, C.E. and SHAW, S.T. PACHIDIS, V., PILIDIS, P.,. MARINAI, L. and TEMPLALEXIS, I. Three-dimensional indicial response of finite aspect ratio yawed wings, pp Towards a full two dimensional gas turbine performance simulator, pp 359-371. 433-442. MANIMALA, B.J., WALKER, D.J., PADFIELD, G.D., VOSKUIJL, M. PADFIELD, G.D., VOSKUIJL, M., GUBBELS, A.W., MANIMALA, and GUBBELS, A.W. B.J. and WALKER, D.J. Rotorcraft simulation modelling and validation for control law design, pp Rotorcraft simulation modelling and validation for control law design, pp 77-88. 77-88. MARINAI, L., TEMPLALEXIS, I., PACHIDIS, V. and PILIDIS, P. PAGE, G.J., MCGUIRK, J.J. and LI, Q. Towards a full two dimensional gas turbine performance simulator, pp Large-eddy simulation of twin impinging jets in cross-flow, pp 195-206. 433-442. PASSMORE, M., RENDER, P. and JOHL, G. MCGUIRK, J.J., LI, Q. and PAGE, G.J. Design and performance of thin, circular arc, wind-tunnel turning vanes, Large-eddy simulation of twin impinging jets in cross-flow, pp 195-206. pp 115-118. MCINTYRE, T.J., KLEINE, H. and HOUWING, A.F.P. PEIRO, J.. CHANTHARASENAWONG, C. and GALVANETTO, U. Optical imaging techniques for hypersonic impulse facilities, pp 1-16. Remarks on the nonlinear dynamics of a typical aerofoil section in dynamic stall, pp 731-739. MCMANUS, H.L., HAGGERTY, A. and MURMAN, E. Lean engineering: a framework for doing the right thing right, pp 105-114. PERHINSCHI, M., CAMPA, G. and NAPOLITANO, MLR. Addressing pose estimation issues for machine vision based UAV MOLLOY, J., WILLIAMS, V., NOLAND, R.B., MAJUMDAR, A., autonomous aerial refuelling, pp 389-396. TOUMI, R. and OCHIENG, W. Reducing environmental impacts of aviation with innovative air traffic PERHINSCHI, M.G. and NAPOLITANO, MLR. management technologies, pp 741-749. Flight data reduction methodology for performance evaluation and comparison of model-following adaptive control laws, pp 807-814. MOORHOUSE, D., RIGGINS, D., TAYLOR, T. and TERHUNE, L. Methods for the design of energy efficient high-speed aerospace vehicles, PILIDIS, P., MARINAT, L., TEMPLALEXIS, I. AND PACHIDIS, V. pp 297-309. Towards a full two dimensionai gas turbine performance simulator, pp 433-442. MORRISON, J., DEARING, S. and LAMBERT, S. Flow control with active dimples, pp 705-714. PILIDIS, P.,. RAMSDEN, K. and KYRITSIS, V.E. The representation of GT component maps using Mach numbers, pp 453-460. MORTON, S.A., CUMMINGS, R.M., FORSYTHE, J.R. and WURTZLER, K. POURTAKDOUST, S.H. and NOBAHARI, H. High resolution computational unsteady aerodynamic techniques applied An optimal-fuzzy two-phase CLOS guidance law design using ant colony to maneouvering UCAVs, pp 397-404. optimisation, pp 621-636. MURMAN, E., MCMANUS, H.L. and HAGGERTY, A. PRICE, M., RAGHUNATHAN, S., BUTTERFIELD, J., GIBSON, A., Lean engineering: a framework for doing the right thing right, pp 105-114. CURRAN, R., CASTAGNE, S. and EARLY, J. Aircraft cost modelling using the genetic causal technique within a NADA, T.R. systems engineering approach, pp 409-420. Performance characterisation of MPD thrusters, pp 443-452. PRITCHARD, D. and MACPHERSON, A. NANGIA, R.K. Strategic Destruction of the Western commercial aircraft sector: ‘Greener’ civil aviation using air-to-air refuelling — relating aircraft design implications of system integration and international risk-sharing business efficiency and tanker offload efficiency, pp 589-592. models, pp 327-334. NAPOLITANO, M.R., PERHINSCHI, M. and CAMPA, G. PYLE, J.A., DESSENS, O. and ROGERS, H.L. Addressing pose estimation issues for machine vision based UAV A change in the calculated impact of supersonic aircraft NOx emissions on autonomous aerial refuelling, pp 389-396. the atmosphere, pp 311-314. NAPOLITANO, M.R. and PERHINSCHI, M.G. PYWELL, M. Flight data reduction methodology for performance evaluation and Developments in RF simulator technology — approaching the affordable comparison of model-following adaptive control laws, pp 807-814. limit, pp 545-560. THE AERONAUTICAL JOURNAL DECEMBER 2007 QIN, N., WONG, W.S. and LE MOIGNE, A. SHAW, S.T. and MANGLANO-VILLAMARIN, C.E. Parallel adjoint-based optimisation of a blended wing body aircraft with Three-dimensional indicial response of finite aspect ratio yawed wings, pp shock control bumps, pp 165-174. 359-371. RADESPIEL, R, YUAN, W., KHALID, M., WINDTE, J. and SCHOLZ, U. SHIVAKUMAR, K.N. and BHARGAVA, A. Computational and experimental investigations of low-Reynolds-number Three dimensional tensile stress concentration in countersunk, pp 777-786. flows past an aerofoil, pp 17-29. SINGH, S. and GHOSH, A.K. RADICE, G. and CASASCO, M. Estimation of lateral-directional parameters using neural networks based On different parameterisation methods to analyse spacecraft attitude modified delta method, pp 659-667. manoeuvres in the presence of attitude constrainsts, pp 335-342. SMART, M. RAGHUNATHAN, S., BUTTERFIELD, J., GIBSON, A., CURRAN, R., Scramjets, pp 605-619. CASTAGNE, S., EARLY, J. and PRICE, M. Aircraft cost modelling using the genetic causal technique within a SMITH, A.D., ELLIOTT, R., DI MARE, L. and IMREGUN, M. systems engineering approach, pp 409-420. A numerical study of high pressure turbine forced response in the presence of damaged nozzle guide vanes, pp 751-757. RAMSDEN, K., KYRITSIS, V.E. and PILIDIS, P. The representation of GT component maps using Mach numbers, pp 453-460. SMITH, H. A review of supersonic businesjse t design issues, pp 761-776. RASI MARZABADI, F. and SOLTANI, MLR. Effect of plunging amplitude on the performance of a wind turbine blade SOLTANI, M.R. and RASI MARZABADL, F. section, pp 571-587. Effect of plunging amplitude on the performance of a wind turbine blade section, pp 571-587. RASUO, B. Some analytical and numerical solutions for the safe turn manoeuvres of SONG, O., KWON, H.D. and LIBRESCU, L. agricultural aircraft — an overview, pp 593-599. Modelling and vibration of an on-classical tilt-rotor wing system, pp 285-295. REED, S.C. STEVENS, J.R.A., BRODIN, G.J. and COOPER, J.A. Development ofa parametric-based indirect aircraft structural usage Measuring the effect of helicopter rotors on GPS reception, pp 561-570. monitoring system using artificial neural networks, pp 209-230. SUNDERLAND, A.G., JOHNSTONE, R. and ALLEN, C.B. RENDER, P., JOHL, G. and PASSMORE, M. Application of a parallel rotor CFD code on HPCx, pp 145-152. Design and performance of thin, circular arc, wind-tunnel turning vanes, pp 115-118. SUNDERLAND, A.J., ASHWORTH, M., BADCOCK, K.J. and EMERSON, D.R. RICHARDSON, G.A., DAWES, W.N. and SAVILL, A.M. High performance computing and computational aerodynamics in the UK, An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion pp 125-131. control analysis, pp 133-144. TANG, H. and ZHONG, S. RICHARDSON, T., LOWENBERG, M., JONES, C. and DUBS, A. A static compressible flow model of synthetic jet actuators, pp 421-431. Dynamic gain scheduled control of aH awk scale model, pp 461-469. TANRIOVER, H. and SENOCAK, E. RIGGINS, D., TAYLOR, T., TERHUNE, L. and MOORHOUSE, D. Analysis of composite plates with variable stiffness using Galerkin Methods for the design of energy efficient high-speed aerospace vehicles, Method, pp 247-255. pp 297-309. TAO, C., DAREN, Y. and WEN, B. ROGERS, H.L., PYLE, J.A. and DESSENS, O. An idea of distributed parameter control for scramjet engines, pp 787-796. A change in the calculated impact of supersonic aircraft NOx emissions on the atmosphere, pp 311-314. TAYLOR, T., TERHUNE, L., MOORHOUSE, D. and RIGGINS, D. Methods for the design of energy efficient high-speed aerospace vehicles, ROMAN, K.M. and HOWELL, R.J. pp 297-309. Loss reduction on ultra high lift low-pressure turbine blades using selective roughness and wake unsteadiness, pp 257-206. TEMPLALEXIS, I., PACHIDIS, V., PILIDIS, P. and MARINAI, L. Towards a full two dimensional gas turbine performance simulator, pp 433-442. ROTARU, M. and BOTEZ, R.M. Relationships between flying qualities and flight tests parameters for the TERHUNE, L., MOORHOUSE, D., RIGGINS, D. and TAYLOR, T. F/A-18 aircraft, pp 281-282. Methods for the design of energy efficient high-speed aerospace vehicles, pp 297-309. SAHA, S. and CHAKRABORTY, D. Numerical exploration of starting process in supersonic nozzle, pp 51-58. TOUMI, R., OCHIENG, W., MOLLOY, J., WILLIAMS, V., NOLAND, R.B. and MAJUMDAR, A. SAVILL, A.M., RICHARDSON, G.A. and DAWES, W.N. Reducing environmental impacts of aviation with innovative air traffic An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion management technologies, pp 741-749. ‘ control analysis, pp 133-144. VOERSMANN, P., GANGULLI, R., JEHNERT, B. and WOLFRAM, J. SAVILL, A.M., RICHARDSON, G.A. and DAWES, W.N. Survivability of helicopter with individual blade primary control failure, An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion pp 645-657. control analysis, pp 133-144. VON BACKSTROM, T.W., INGHAM, L.A., MANESCHIJN, A. and SCHOLZ, U., RADESPIEL, R., YUAN, W., KHALID, M. and JONES, T. WINDTE, J. A proposed reference framework for unmanned aerial vehicle and system Computational and experimental investigations of low-Reynolds-number airworthiness requirements, pp 345-358. flows past an aerofoil, pp 17-29. VOSKUIJL, M., GUBBELS, A.W., MANIMALA, B.J., WALKER, D.J. SENOCAK, E. and TANRIOVER, H. and PADFIELD, G.D. Analysis of composite plates with variable stiffness using Galerkin Rotorcraft simulation modelling and validation for control law design, pp Method, pp 247-255. 77-88. INDEX TO VOLUME 111 WALKER, D.J., PADFIELD, G.D., VOSKUIJL, M., GUBBELS, A.W. WU, W.H., WANG, J.J., HUANG, Y. and CHEN, D.H. and MANIMALA, B.J. Investigation on the aerodynamic performance on an ejection seat, pp 373- Rotorcraft simulation modelling and validation for control law design, pp 380. 77-88. WURTZLER, K., MORTON, S.A., CUMMINGS, R.M. and WANG, J.J., HUANG, Y., CHEN, D.H. and WU, W.H. FORSYTHE, J.R. Investigation on the aerodynamic performance on an ejection seat, pp 373-380. High resolution computational unsteady aerodynamic techniques applied to maneouvering UCAVs, pp 397-404. WATSON, M., JAWORSKI, A.J. and WOOD, N.J. Application of synthetijce ta ctuators for the modification of the YOUBI, Z. and T. ZEBBICHE characteristics of separated shear layers on slender wings, pp 519-529. Effect of stagnation temperature on supersonic flow parameters application for air in nozzles, pp 31-40. WEN, B., TAO, C. and DAREN, Y., YUAN, K. and CAO, Y. An idea ofd istributed parameter control for scramjet engines, pp 787-796. Aircraft flight characteristics in conditions of windshear and icing, pp 41- 49. WILLIAMS, V., NOLAND, R.B., MAJUMDAR, A., TOUML, R., OCHIENG, W. and MOLLOY, J. YUAN, W., KHALID, M., WINDTE, J., SCHOLZ, U. and Reducing environmental impacts of aviation with innovative air traffic RADESPIEL, R. management technologies, pp 741-749. Computational and experimental investigations of low-Reynolds-number flows past an aerofoil, pp 17-29. WINDTE, J., SCHOLZ, U., RADESPIEL, R, YUAN, W. and KHALID, M. Computational and experimental investigations of low-Reynolds-number ZEBBICHE, T. and YOUBI, Z. flows past an aerofoil, pp 17-29. Effect of stagnation temperature on supersonic flow parameters application for air in nozzles, pp 31-40. WOLFRAM, J., VOERSMANN, P., GANGULI, R. and JEHNERT, B. Survivability of helicopter with individual blade primary control failure, ZHONG, S. and GUO, F. pp 645-657. A PIV investigation of the characteristics of micro-scale synthetic jets, pp 509-518. WONG, W.S., LE MOIGNE, A. and QIN, N. Parallel adjoint-based optimisation of a blended wing body aircraft with ZHONG, S. and TANG, H. shock control bumps, pp 165-174. A static compressible flow model of synthetijce t actuators, pp 421-431. WOOD, N.J., WATSON, M. and JAWORSKI, A.J. ZHU, G., BEARMAN, P.W. and GRAHAM, J.MLR. Application of syntheticje t actuators for the modification of the Prediction of drag and lift of wings from velocity and vorticity fields, pp characteristics of separated shear layers on slender wings, pp 519-529. 699-704. Volume CXI Number 1115 January pp 1-58 Number 1116 February pp 61-122 Number 1117 March pp 125-206 Number 1118 April pp 209-282 Number 1119 May pp 285-342 Number 1120 June pp 345-406 Number 1121 July pp 409-471 Number 1122 August pp 473-542 Number 1123 September pp 545-603 Number 1124 October pp 605-670 Number 1125 November pp 673-757 Number 1126 December pp 761-828

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INDEX TO VOLUME 111 THE AERONAUTICAL JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY Volume CXl January-December 2007 Subject Index AERODYNAMICS AIR TRAFFIC MANAGEMENT A message from the editor. P. Bearman, November pp iv. Reducing environmental impacts of aviation with innovative air traffic A PIV investigation of the characteristics of micro-scale synthetic jets. management technologies. V. Williams, R.B. Noland, A. F. Guo and S. Zhong, pp 509-518. Majumdar, R. Toumi, W. Ochieng and J. Molloy, pp 741-749. Computational and experimental investigations of low-Reynolds- number flows past an aerofoil. W. Yuan, M. Khalid, J. Windte, U. AIRCRAFT DESIGN Scholz and R. Radespiel, pp 17-29. A review of supersonic businesjse t design issues. H. Smith, pp 761- Effect of plunging amplitude on the performance of a wind turbine 776. blade section. M.R. Soltani and F. Rasi Marzabadi, pp 571-587. Flow control with active dimples. S. Dearing, S. Lambert and J. AIRWORTHINESS Morrison, pp 705-714. A proposed reference framework for unmanned aerial vehicle and High performance computing and computational aerodynamics in the system airworthiness requirements. A. Maneschijn, T. Jones, T.W. UK. D.R. Emerson, A.J. Sunderland, M. Ashworth and K._J. von Backstrém and L.A. Ingham, pp 345-358. Badcock, pp 125-131. Investigation on the aerodynamic performance on an ejection seat. BOOK REVIEWS — BY AUTHOR D.H. Chen, W.H. Wu, J.J. Wang and Y. Huang, pp 373-380. Aliabadi, M.H. and Guagliano, M. Fractures and Damage of Large-eddy simulation of separated flow over a swept wing with Composites, p 826. approximate near-wall modelling. N. Li and M.A. Leschziner, pp Anderson, J.D. Hypersonic and High Temperature Gas Dynamics, 689-697. Second Edition, p 121. Large-eddy simulation of twin impinging jets in cross-flow. Q. Li, Armstrong, K.B. et a/ Care and Repair of Advanced Composites, G.J. Page and J.J. McGuirk, pp 195-206. Second Edition, p 120. Parallel adjoint-based optimisation of a blended wing body aircraft Borgnakke, C. and Sonntag, R.E. Introduction to Engineering with shock control bumps. W.S. Wong, A. Le Moigne and N. Qin, Thermodynamics, Second Edition, p 122. pp 165-174. Cloud, M.J. and Moore, R.E. Computational Functional Aanlysis, Prediction of aerodynamic forces on a helicopter fuselage. A. Second Edition, p 603. Filippone, pp 175-184. Curtis, P., Kuhn, R.F.E. and Margason, R.J. Jet Induced Effects: the Prediction of drag and lift of wings from velocity and vorticity fields. Aerodynamics of Jet and Fan Powered V/STOL Aircraft in Hover G. Zhu, P.W. Bearman and J.M.R. Graham, pp 699-704. and Transition, p 670. Remarks on the nonlinear dynamics of a typical aerofoil section in Dodson, B. and Schwab, H. Accelerated Testing; a Practioner’s Guide dynamic stall. U. Galvanetto, J. Peiro and C. Chantharasenawong, to Accelerated and Reliability Testing, p 119. pp 731-739. Dowell, E.H. (Ed) et al A Modern Course in Aeroelasticity, Fourth The onset of compressibility effects for aerofoils in ground effect. Edition, p 120. Technical note, G. Doig, T.J. Barber, E. Leonardi and A.J. Neely, Dreier, M.E. Introduction to Helicopter and Tiltrotor Flight pp 797-806. Simulation, p 405. Fillippone, A. Flight Performance of Fixed and Rotary Wing Aircraft, AEROSPACE ENGINEERING p 603. New commercial opportunities in space. D.M. Ashford, pp 61-75. Fisher, L.W. Selection of Engineering Materials and Adhesives, p On different parameterisation methods to analyse spacecraft attitude 471. manoeuvres in the presence of attitude constrainsts. G. Radice and Flack, J.D. Fundamentals uf Jet Propulsion with Applications, p 470. M. Casasco, pp 335-342. Fleeman, E.L. Tactical Missile Design, Second Edition, p 119. Performance characterisation of MPD thrusters. T.R. Nada, Guagliano, M. and Aliabadi, M.H. Fractures and Damage of pp 443. Composites, p 826. 816 THE AERONAUTICAL JOURNAL DECEMBER 2007 Henderson, D.M. Applied Cartesian Tensors for Aerospace Tischler, M.B. and Remple, R.K. Aircraft and Rotorcraft System Simulators, p 121. Identification: Engineering Methods with Flight Test Examples, p 601. Howe, M.S. Hydrodynamics and Sound, p 668. Ugaral, A.C. Mechanics of Materials, p 740. Jategaonkar, R.V. Flight Vehicle System Identification: a Time Wagg, D. (Ed) et al. Adaptive Structures: Engineering Applications, p Domain Methodology. Progess in Aeronautics and Astronautics 827. series Vol 216, p 601. Wiley, R.G. ELINT: the Interception and Analysis of Radar Signals, p Kiusalaas, J. Numerical Methods in Engineering with MATLAB, p 280. 280. Kiusalaas, J. Numerical Methods in Engineering with Python, p 280. Zarchan, P. Tactical and Strategic Missile Guidance, Fifth Edition, Klein, V. and Morelli, E.A. Aircraft System Identification: Theory and Progress in Aeronautics and Astronautics series Vol 219, p 406, Practice, p 602. 470. Knight, D.D. Elements of Numerical Methods for Compressibility Flows, p 740. BOOK REVIEWS — BY TITLE Kraige, L.G. and Meriam, J.L. Engineering Mechanics (Vol 2) — A Modern Course in Aeroelasticity, Fourth Edition, E.H. Dowell (Ed) Dynamics, Sixth Edition, p 406. etal, p 120. Krysinski, T. and Malburet, F. Mechanical Vibrations: Active and Adaptive Structures: Engineering Applications, D. Wagg (Ed) et al, p Passive Control, p 668 827. Kuhn, R.F.E., Margason, R.J. and Curtis, P. Jet Induced Effects: the Accelerated Testing; a Practioner’s Guide to Accelerated and Aerodynamics of Jet and Fan Powered V/STOL Aircraft in Hover Reliability Testing, B. Dodson and H. Schwab, p 119. and Transition, p 670. Advanced Vector Analysis for Scientists and Engineers, M. Rahman, Kutz, M. (Ed) Environmentally Conscious Mechanical Design, p 669. p 668. Kutz, M. (Ed) Environmentally Conscious Manufacturing, p 670. Aircraft and Rotorcraft System Identification: Engineering Methods Leishmann, J.G. Principles of Helicopter Aerodynamics, Second with Flight Test Examples, M.B. Tischler and R.K. Remple, p 601. edition, p 825. Aircraft Design — a Conceptual Approach, Fourth Edition, D.P. Levin, E.M. Dynamic Analysis of Space Tether Missions. American Raymer, p 120. Astronautical Society (AAS) Advances in the Astronautical Aircraft Performance, M. Saarlas, p 669. Sciences series Vol 126, p 750. Aircraft System Identification: Theory and Practice, V. Klein and E.A. Lorenz, R.D. Spinning Flight: Dynamics of Frisbees, Boomerangs, Morelli, p 602. Samaras and Skipping Stones, p 122. Applied Cartesian Tensors for Aerospace Simulators, D.M. Malburet, F. and Krysinski, T. Mechanical Vibrations: Active and Henderson, p 121. Passive Control, p 668. Care and Repair of Advanced Composites, Second Edition, K.B. Margason, R.J., Curtis, P. and Kuhn, R.F.E. Jet Induced Effects: the Armstrong et al, p 120. Aerodynamics of Jet and Fan Powered V/STOL Aircraft in Hover Computational Functional Analysis, Second Edition, R.E. Moore and and Transition, p 670. M.J. Cloud, p 603. Mattingly, J.D. Elements of Propulsion: Gas Turbines and Rockets, Dynamic Analysis of Space Tether Missions. American Astronautical Second Edition, p 119. Society (AAS) Advances in the Astronautical Sciences series Vol Meriam, J.L. and Kraige, L.G. Engineering Mechanics (Vol 2) — 126, E.M. Levin, p 750. Dynamics, Sixth Edition, p 406. Elements of Numerical Methods for Compressibility Flows, D.D. Moore, R.E. and Cloud, M.J. Compuiational Functional Aanlysis, Knight, p 740. Second Edition, p 603. Elements of Propulsion: Gas Turbines and Rockets, Second Edition, Moran, M.J. and Shapiro, H.N. Fundamentals of Engineering J.D. Mattingly, p 119. Thermodynamics, Fifth Edition, p 122. ELINT: the Interception and Analysis of Radar Signals, R.G. Wiley, p Morelli, E.A. and Klein, V. Aircraft System Identification: Theory and 280. Practice, p 602. Engineering Mechanics (Vol 2) — Dynamics, Sixth Edition, J.L. Mueller, T.J. et al Introduction to the Design of Fixed-Wing Micro Meriam and L.G. Kraige, p 406. Air Vehicles: including Three Case Studies, p 405. Environmentally Conscious Manufacturing, M. Kutz (Ed), p 670. Pai, P.F. Highly Flexible Structures: Modeling, Computation and Environmentally Conscious Mechanical Design, M. Kutz (Ed), p 669. Experimentation, p 826. Flight Performance of Fixed and Rotary Wing Aircraft, A. Fillippone, Rahman, M. Advanced Vector Analysis for Scientists and Engineers, p 603. p 668. Flight Vehicle System Identification: a Time Domain Methodology. Raymer, D.P. Aircraft Design - a Conceptual Approach, Fourth Progess in Aeronautics and Astronautics series Vol 216, R.V. Edition, p 120. Jategaonkar, p 601. Raymer, D.P. RDS-Student: Sofrtware for Aircraft Design, Sizing and Fractures and Damage of Composites. M. Guagliano and M.H Performance, p 120. Aliabadi, p 826. Remple, R.K. and Tischler, M.B. Aircraft and Rotorcraft System Fundamentals of Engineering Thermodynamics, Fifth Edition, M.J. Identification: Engineering Methods with Flight Test Examples, p Moran and H.N. Shapiro, p 122. 601. Fundamentals of Jet Propulsion with Applications, J.D. Flack, p 470. Saarlas, M. Aircraft Performance, p 669. Health Monitoring of Aerospace Structures: Smart Sensor Schwab, H. and Dodson, B. Accelerated Testing; a Practioner’s Guide Technologies and Signal Processing, W. Staszewski et al, p 750. to Accelerated and Reliability Testing, p 119. Highly Flexible Structures: Modeling, Computation and Shapiro, H.N. and Moran, M.J. Fundamentals of Engineering Experimentation. P.F. Pai, p 826. Thermodynamics, Fifth Edition, p 122. Hydrodynamics and Sound, M.S. Howe, p 668. Sonntag, R.E. and Borgnakke, C. Introduction to Engineering Hypersonic and High Temperature Gas Dynamics, Second Edition, Thermodynamics, Second Edition, p 122. J.D. Anderson, p 121. Staszewski, W. ef al Health Monitoring of Aerospace Structures: Introduction to Engineering Thermodynamics, Second Edition, R.E. Smart Sensor Technologies and Signal Processing, p 750. Sonntag and C. Borgnakke, p 122. INDEX TO VOLUME 111 Introduction to Helicopter and Tiltrotor Flight Simulation, M.E. Large-eddy simulation of separated flow over a swept wing with Dreier, p 405. approximate near-wall modelling. N. Li and M.A. Leschziner, pp Introduction to the Design of Fixed-Wing Micro Air Vehicles: 689-697. including Three Case Studies, T.J. Mueller ef al, p 405. Numerical study of transonic cavity flows using large-eddy and Jet Induced Effects: the Aerodynamics of Jet and Fan Powered detached-eddy simulation. P. Nayyar, G.N. Barakos and K.J. V/STOL Aircraft in Hover and Transition, R.F.E. Kuhn, R.J. Badcock, pp 153-164. Margason and P. Curtis, p 670. Parallel adjoint-based optimisation of ab lended wing body aircraft Mechanical Vibrations: Active and Passive Control, T. Krysinski and with shock control bumps. W.S. Wong, A. Le Moigne and N. Qin, F. Malburet, p 668. pp 165-174. Mechanics of Materials, A.C. Ugaral, p 740. The representation ofG T component maps using Mach numbers. V.E. Numerical Methods in Engineering with MATLAB, J. Kiusalaas, p Kyritsis, P. Pilidis and K. Ramsden, pp 453-460. 280. Three-dimensional indicial response of finite aspect ratio yawed Numerical Methods in Engineering with Python, J. Kiusalaas, p 280. wings. C.E. Manglano-Villamarin and S.T. Shaw, pp 359-371. Principles of Helicopter Aerodynamics, Second edition. J.G. Towards a full two dimensional gas turbine performance simulator. V. Leishmann, p 825. Pachidis, P. Pilidis, L. Marinai and I. Templalexis, pp 433-442. RDS-Student: Sofrtware for Aircraft Design, Sizing and Performance, D.P. Raymer, p 120. DESIGN Selection of Engineering Materials and Adhesives, L.W. Fisher, p Design of fixed wing micro air vehicles. P. Cosyn, pp 315-326. 471. On the benefits of lower Mach number aircraft cruise. A. Filippone, Spinning Flight: Dynamics of Frisbees, Boomerangs, Samaras and pp 531-542. Skipping Stones, R.D. Lorenz, p 122. Tactical and Strategic Missile Guidance, Fifth Edition, Progress in ENVIRONMENTAL ENGINEERING Aeronautics and Astronautics series Vol 219, P. Zarchan, p 406, Lean engineering: a framework for doing the right thing right. H.L. 470. McManus, A. Haggerty and E. Murman, pp 105-114. Tactical Missile Design, Second Edition, E.L. Fleeman, p 119, A change in the calculated impact of supersonic aircraft NOx emissions on the atmosphere. O. Dessens, H.L. Rogers and J.A. COMPOSITES Pyle, pp 311-314. A study of secondary instabilities in postbuckling composite ‘Greener’ civil aviation using air-to-air refuelling — relating aircraft aerostructures. B.G. Falzon and M. Cerini, pp 715-729. design efficiency and tanker offload efficiency. R.K. Nangia, pp Analysis of composite plates with variable stiffness using Galerkin 589-592. Method. E. Senocak and H. Tanriover, pp 247-255. On the benefits of lower Mach number aircraft cruise. A. Filippone, pp 531-542. COMPUTATIONAL FLUID DYNAMICS Reducing environmental impacts of aviation with innovative air traffic Achieving high parallel performance for an unstructured unsteady management technologies. V. Williams, R.B. Noland, A. turbomachinery CFD code. N. Hills, pp 185-193. Majumdar, R. Toumi, W. Ochieng and J. Molloy, pp 741-749. An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion control analysis. A.M. Savill, G.A. Richardson and W.N. FLIGHT CONTROL DYNAMICS Dawes, pp 133-144. Aircraft flight characteristics in conditions of windshear and icing. Y. Application of a parallel rotor CFD code on HPCx. C.B. Allen, A.G. Cao and K. Yuan, pp 41-49. Sunderland and R. Johnstone, pp 145-152. Dynamic gain scheduled control of aH awk scale model. T. Computational and experimental investigations of low-Reynolds- Richardson, M. Lowenberg, C. Jones and A. Dubs, pp 461-469. number flows past an aerofoil. W. Yuan, M. Khalid, J. Windte, U. Estimation of lateral-directional parameters using neural networks based Scholz, and R. Radespiel, pp 17-29. modified delta method. S. Singh and A. K. Ghosh, pp 659-667. High performance computing and computational aerodynamics in the Relationships between flying qualities and flight tests parameters for UK. D.R. Emerson, A.J. Sunderland, M. Ashworth and K.J. the F/A-18 aircraft. R.M. Botez and M. Rotaru, pp 281-282. Badcock, pp 125-131. Some analytical and numerical solutions for the safe turn manoeuvres The onset of compressibility effects for aerofoils in ground effect. of agricultural aircraft — an overview. B. Rasuo, pp 593-599. Technical note, G. Doig, T.J. Barber, E. Leonardi and A.J. Neely, pp 797-806. FLIGHT SIMULATION Addressing pose estimation issues for machine vision based UAV COMPUTATIONAL TECHNIQUES autonomous aerial refuelling. G,C ampa, M.R. Napolitano and M. A static compressible flow model of synthetijce t actuators. H. Tang Perhinschi, pp 389-396. and S. Zhong, pp 421-431. Aircraft cost modelling using the genetic causal technique within a FLIGHT TEST systems engineering approach. R. Curran, S. Castagne, J. Early, Relationships between flying qualities and flight tests parameters for M. Price, S. Raghunathan, J. Butterfield and A. Gibson, pp 409- the F/A-18 aircraft. R.M. Botez and M. Rotaru, pp 281-282. 420. Experimental and computational study of unsteady hypersonic cavity HISTORY flows. S. Creighton and R. Hillier, pp 673-688. The Victoria University of Manchester’s contributions to the Flight data reduction methodology for performance evaluation and development of aeronautics. J.A.D. Ackroyd, pp 473-493. comparison of model-following adaptive control laws. M.G. Perhinschi and M.R. Napolitano, pp 807-814. INDUSTRY High resolution computational unsteady aerodynamic techniques Strategic Destruction of the Western commercial aircraft sector: applied to maneouvering UCAVs. S.A. Morton, R.M. Cummings, implications of system integration and international risk-sharing J.R. Forsythe and K. Wurtzler, pp 397-404. business models. D. Pritchard and A. MacPherson, pp 327-334. 818 THE AERONAUTICAL JOURNAL DECEMBER 2007 JETS STRUCTURES A PIV investigation of the characteristics of micro-scale synthetic jets. A study of secondary instabilities in postbuckling composite F. Guo and S. Zhong, pp 509-518. aerostructures. B.G. Falzon and M. Cerini, pp 715-729. A static compressible flow model of synthetic jet actuators. H. Tang Analysis of composite plates with variable stiffness using Galerkin and S. Zhong, pp 421-431. Method. E. Senocak and H. Tanriover, pp 247-255. Application of synthetic jet actuators for the modification of the Development of a parametric-based indirect aircraft structural usage characteristics of separated shear layers on slender wings. M. monitoring system using artificial neural networks. S.C. Reed, pp Watson, A.J. Jaworski and N.J. Wood, pp 519-529. 209-230. Large-eddy simulation of twin impinging jets in cross-flow. Q. Li, Three dimensional tensile stress concentration in countersunk. A. G.J. Page and J.J. McGuirk, pp 195-206. Bhargava and K. N. Shivakumar, pp 777-786. LIGHTER THAN AIR SYSTEMS Performance of non-rigid airships operating in the neutral buoyancy An optimal-fuzzy two-phase CLOS guidance law design using ant condition. G.E. Dorrington, pp 89-103. colony optimisation. H. Nobahari and S.H. Pourtakdoust, pp 621- 636. PROPULSION Development of a parametric-based indirect aircraft structural usage A numerical study of high pressure turbine forced response in the monitoring system using artificial neural networks. S.C. Reed, pp presence of damaged nozzle guide vanes. L. di Mare, M. Imregun, 209-230. A.D. Smith and R. Elliott, pp 751-757. Developments in RF simulator technology — approaching the Achieving high parallel performance for an unstructured unsteady affordable limit. M. Pywell, pp 545-560. turbomachinery CFD code. N. Hills, pp 185-193. Measuring the effect of helicopter rotors on GPS reception. G.J. An idea ofd istributed parameter control for scramjet engines. Y. Brodin, J.A. Cooper and J.R.A. Stevens, pp 561-570. Daren, C. Tao and B. Wen, pp 787-796. An unsteady, moving mesh CFD simulation for Harrier hot-gas The MIL-STD-1553B data bus: What does the future hold? D.R. ingestion control analysis. A.M. Savill, G.A. Richardson and W.N. Bracknell, pp 231-246. Dawes, pp 133-144. Use of Global Positioning System velocity outputs for determining Effect of stagnation temperature on supersonic flow parameters airspeed measurement error. G.B. Gratton, pp 381-388. application for air in nozzles. T. Zebbiche and Z. Youbi, pp 31-40. Loss reduction on ultra high lift low-pressure turbine blades using TESTING FACILITIES AND TECHNOLOGIES selective roughness and wake unsteadiness. R.J. Howell and K.M. A review of some current research on pressure sensitive paint and Roman, pp 257-206. thermographic phosphor techniques. K. Kontis, pp 495-508. Methods for the design of energy efficient high-speed aerospace vehicles. Design and performance of thin, circular arc, wind-tunnel turning D. Riggins, T.Taylor, L. Terhune and D. Moorhouse, pp 297-309. vanes. G. Johl, M. Passmore and P. Render, pp 115-118. Numerical exploration of starting process in supersonic nozzle. S. Developments in RF simulator technology — approaching the Saha and D. Chakraborty, pp 51-58. affordable limit. M. Pywell, pp 545-560. Performance characterisation of MPD thrusters. T.R. Nada, pp 443-452. Experimental and computational study of unsteady hypersonic cavity Scramjets. M. Smart, pp 605-619. flows. S. Creighton and R. Hillier, pp 673-688. The representation of GT component maps using Mach numbers. V.E. Optical imaging techniques for hypersonic impulse facilities. T.J. ‘Kyritsis, P. Pilidis and K. Ramsden, pp 453-460. McIntyre, H. Kleine and A.F.P. Houwing, pp 1-16. Towards a full two dimensional gas turbine performance simulator. V. Pachidis, P. Pilidis, L. Marinai and I. Templalexis, pp 433-442. TRAINING A systems approach to training aeronautical decision making: from ROTORCRAFT identifying training needs to verifying training solutions. D. Harris Modelling and vibration ofa non-classical tilt-rotor wing system. O. and W.-C. Li, pp 267-279. Song, H.D. Kwon and L. Librescu, pp 285-295. Application of a parallel rotor CFD code on HPCx. C.B. Allen, A.G. UNMANNED AIR VEHICLES Sunderland and R. Johnstone, pp 145-152. A proposed reference framework for unmanned aerial vehicle and Measuring the effect of helicopter rotors on GPS reception. G.J. system airworthiness requirements. A. Maneschijn, T. Jones, T.W. Brodin, J.A. Cooper and J.R.A. Stevens, pp 561-570. von Backstrém and L.A. Ingham, pp 335-342. Modelling the interaction of helicopter main rotor and tail rotor wakes. Addressing pose estimation issues for machine vision based UAV T.M. Fletcher and R.E. Brown, pp 637-643. autonomous aerial refuelling. G,C ampa, M.R. Napolitano and M. Prediction of aerodynamic forces on a helicopter fuselage. A. Filippone, pp 175-184. Perhinschi, pp 389-396. Rotorcraft simulation modelling and validation for control law design. Design of fixed wing micro air vehicles. P. Cosyn, pp 315-326. B.J. Manimala, D.J. Walker, G.D. Padfield, M. Voskuijl and A.W. High resolution computational unsteady aerodynamic techniques Gubbels, pp 77-88. applied to maneouvering UCAVs. S.A. Morton, R.M. Cummings, Survivability of helicopter with individual blade primary control failure. J.R. Forsythe and K. Wurtzler, pp 397-404. R. Ganguli, B. Jehnert, J. Wolfram and P. Voersmann, pp 645-657. VIBRATION SIMULATION Modelling and vibration of a non-classical tilt-rotor wing system. O. Aircraft flight characteristics in conditions of windshear and icing. Y. Song, H.D. Kwon and L. Librescu, pp 285-295. Cao and K. Yuan, pp 41-49. Rotorcraft simulation modelling and validation for control law design. WAKES B.J. Manimala, D.J. Walker, G.D. Padfield, M. Voskuijl and A.W. Modelling the interaction of helicopter main rotor and tail rotor wakes. Gubbels, pp 77-88. T.M. Fletcher and R.E. Brown, pp 637-643. INDEX TO VOLUME 111 Author Index ACKROYD, J.A.D. CASTAGNE, S., EARLY, J., PRICE, M., RAGHUNATHAN, S., The Victoria University of Manchester’s contributions to the development BUTTERFIELD, J., GIBSON, A. and CURRAN, R. of aeronautics, pp 473-493. Aircraft cost modelling using the genetic causal technique within a systems engineering approach, pp 409-420. ALLEN, C.B., SUNDERLAND, A.G. and JOHNSTONE, R. Application of a parallel rotor CFD code on HPCx, pp 145-152. CERINI, M. and FALZON, B.G. A study of secondary instabilities in postbuckling composite ASHFORD, D.M. aerostructures, pp 715-729. New commercial opportunities in space, pp 61-75. CHAKRABORTY, D. and SAHA, S. ASHWORTH, M. and BADCOCK, K.J., EMERSON, D.R. and Numerical exploration of starting process in supersonic nozzle, pp 51-58. SUNDERLAND, A.J. High performance computing and computational aerodynamics in the UK, CHANTHARASENAWONG, C., GALVANETTO, U. and PEIRO, J. pp 125-131. Remarks on the nonlinear dynamics of a typical aerofoil section in dynamic stall, pp 731-739. BADCOCK, K.J., EMERSON, D.R., SUNDERLAND, A.J. and ASHWORTH, M. CHEN, D.H., WU, W.H., WANG, J.J. and HUANG, Y. High performance computing and computational aerodynamics in the UK, Investigation on the aerodynamic performance on an ejection seat, pp 373-380. pp 125-131. COOPER, J.A., STEVENS, J.R.A. and RRODIN, G.J. BADCOCK, K.J., NAYYAR, P. and BARAKOS, G.N. Measuring the effect of helicopter rotors on GPS reception, pp 561-570. Numerical study of transonic cavity flows using large-eddy and detached- eddy simulation, pp 153-164. COSYN, P. Design of fixed wing micro air vehicles, pp 315-326. BARAKOS, G.N., BADCOCK, K.J. and NAYYAR, P. Numerical study of transonic cavity flows using large-eddy and detached- CREIGHTON, S. and HILLIER, R. eddy simulation, pp 153-164. Experimental and computational study of unsteady hypersonic cavity flows, pp 673-688. BARBER, T.J., LEONARDI, E., NEELY, A.J. and DOIG, G. The onset of compressibility effects for aerofoils in ground effect, Technical CUMMINGS, R.M., FORSYTHE, J.R., WURTZLER, K. and note, pp 797-806. MORTON, S.A. High resolution computational unsteady aerodynamic techniques applied BEARMAN, P.W. to maneouvering UCAVs, pp 397-404. A message from the editor, November pp iv. CURRAN, R., CASTAGNE, S., EARLY, J., PRICE, M., BEARMAN, P.W., GRAHAM, J.M.R. and ZHU, G. RAGHUNATHAN, S., BUTTERFIELD, J. and GIBSON, A. Prediction of drag and lift of wings from velocity and vorticity fields, pp Aircraft cost modelling using the genetic causal technique w ithin a 699-704. systems engineering approach, pp 409-420. BHARGAVA, A. and SHIVAKUMAR, K.N. DAREN, Y., WEN, B. and TAO, C. Three dimensional tensile stress concentration in countersunk, pp 777-786. An idea of distributed parameter control for scramjet engines, pp 787-796 BOTEZ, R.M. and ROTARU, M. DEARING, S., LAMBERT, S. and MORRISON, J. Relationships between flying qualities and flight tests parameters for the Flow control with active dimples, pp 705-714. F/A-18 aircraft, pp 281-282. DESSENS, O., ROGERS, H.L. and PYLE, J.A. BRACKNELL, D.R. A change in the calculated impact of supersonic aircraft NOx emissions on The MIL-STD-1553B data bus: What does the future hold?, pp 231-246. the atmosphere, pp 311-314. BRODIN, G.J., COOPER, J.A. and STEVENS, J.R.A. DI MARE, L., IMREGUN, M., SMITH, A.D. and ELLIOTT, R. Measuring the effect of helicopter rotors on GPS reception, pp 561-570. A numerical study of high pressure turbine forced response in the presence of damaged nozzle guide vanes, pp 751-757. BROWN, R.E. and FLETCHER, T.M. Modelling the interaction of helicopter main rotor and tail rotor wakes, pp DOIG, G., BARBER, T.J., LEONARDI, E. and NEELY, A.J. 637-643. The onset of compressibility effects for aerofoils in ground effect, Technical note, pp 797-806. BUTTERFIELD, J., GIBSON, A., CURRAN, R., CASTAGNE, S., EARLY, J., PRICE, M. and RAGHUNATHAN, S. DORRINGTON, G.E. Aircraft cost modelling using the genetic causal technique within a Performance of non-rigid airships operating in the neutral buoyancy systems engineering approach, pp 409-420. condition, pp 89-103. CAMPA, G., NAPOLITANO, M.R. and PERHINSCHI, M. DUBS, A., RICHARDSON, T., LOWENBERG, M. and JONES, C. Addressing pose estimation issues for machine vision based UAV Dynamic gain scheduled control of aH awk scale model, pp 461-469. autonomous aerial refuelling, pp 389-396. EARLY, J., PRICE, M., RAGHUNATHAN, S., BUTTERFIELD, J., CAO, Y. and YUAN, K. GIBSON, A., CURRAN, R. and CASTAGNE, S. Aircraft flight characteristics in conditions of windshear and icing, pp 41- Aircraft cost modelling using the genetic causal technique within a 49. systems engineering approach, pp 409-420. CASASCO, M. and RADICE, G. ELLIOTT, R., DI MARE, L., IMREGUN, M. and SMITH, A.D. On different parameterisation methods to analyse spacecraft attitude A numerical study of high pressure turbine forced response in the presence manoeuvres in the presence of attitude constrainsts, pp 335-342. of damaged nozzle guide vanes, pp 751-757. 820 THE AERONAUTICAL JOURNAL DECEMBER 2007 EMERSON, D.R., SUNDERLAND, A.J., ASHWORTH, M. and HUANG, Y., CHEN, D.H., WU, W.H. and WANG, J.J. BADCOCK, K.J. Investigation on the aerodynamic performance on an ejection seat, pp 373-380. High performance computing and computational aerodynamics in the UK, pp 125-131. IMREGUN, M., SMITH, A.D., ELLIOTT, R. and DI MARE, L. A numerical study of high pressure turbine forced response in the presence FALZON, B.G. and CERINI, M. of damaged nozzle guide vanes, pp 751-757. A study of secondary instabilities in postbuckling composite aerostructures, pp 715-729. INGHAM, L.A., MANESCHIJN, A., JONES, T. and VON BACKSTROM, T.W. FILIPPONE, A. A proposed reference framework for unmanned aerial vehicle and system Prediction of aerodynamic forces on a helicopter fuselage, pp 175-184. airworthiness requirements, pp 345-358. FILIPPONE, A. JAWORSKI, A.J., WOOD, N.J. and WATSON, M. On the benefits of lower Mach number aircraft cruise, pp 531-542. Application of synthetic jet actuators for the modification of the characteristics of separated shear layers on slender wings, pp 519-529. FLETCHER, T.M. and BROWN, R.E. Modelling the interaction of helicopter main rotor and tail rotor wakes, pp JEHNERT, B., WOLFRAM, J.,. VOERSMANN, P. and GANGULI, R. 637-643. Survivability of helicopter with individual blade primary control failure, pp 645-657. FORSYTHE, J.R., WURTZLER, K., MORTON, S.A. and CUMMINGS, R.M. JOHL, G., PASSMORE, M. and RENDER, P. High resolution computational unsteady aerodynamic techniques applied Design and performance oft hin, circular arc, wind-tunnel turning vanes, to maneouvering UCAVs, pp 397-404. pp 115-118. GALVANETTO, U., PEIRO, J. and CHANTHARASENAWONG, C. JOHNSTONE, R., ALLEN, C.B. and SUNDERLAND, A.G. Remarks on the nonlinear dynamics of a typical aerofoil section in Application of a parallel rotor CFD code on HPCx, pp 145-152. dynamic stall, pp 731-739. JONES, C., DUBS, A., RICHARDSON, T. and LOWENBERG, M. GANGULL, R., JEHNERT, B., WOLFRAM, J. and VOERSMANN, P. Dynamic gain scheduled control of aH awk scale model, pp 461-469. Survivability of helicopter with individual blade primary control failure, pp 645-657. JONES, T., VON BACKSTROM, T.W., INGHAM, L.A. and MANESCHIJN, A. s GHOSH, A.K. and SINGH, S. A proposed reference framework for unmanned aerial vehicle and system Estimation of lateral-directional parameters using neural networks based airworthiness requirements, pp 345-358. modified delta method, pp 659-667. KHALID, M., WINDTE, J., SCHOLZ, U., RADESPIEL, R. and YUAN, W. GIBSON, A., CURRAN, R., CASTAGNE, S., EARLY, J., PRICE, M., Computational and experimental investigations of low-Reynolds-number RAGHUNATHAN, S. and BUTTERFIELD, J. flows past an aerofoil, pp 17-29. Aircraft cost modelling using the genetic causal technique within a systems engineering approach, pp 409-420. KLEINE, H, HOUWING, A.F.P. and MCINTYRE, T.J., Optical imaging techniques for hypersonic impulse facilities, pp 1-16. GRAHAM, J.M.R., ZHU, G. and BEARMAN, P.W. Prediction of drag and lift of wings from velocity and vorticity fields, pp KONTIS, K. 699-704. A review of some current research on pressure sensitive paint and thermographic phosphor techniques, pp 495-508. GRATTON, G.B. Use of Global Positioning System velocity outputs for determining KWON, H.D., LIBRESCU, L. and SONG, O. airspeed measurement error, pp 381-388. Modelling and vibration of a non-classical tilt-rotor wing system, pp 285- 295. GUBBELS, A.W., MANIMALA, B.J., WALKER, D.J., PADFIELD, G.D. and VOSKUIJL, M. KYRITSIS, V.E., PILIDIS, P. and RAMSDEN, K. Rotorcraft simulation modelling and validation for control law design, pp 77-88. The representation ofG T component maps using Mach numbers, pp 453-460. GUO, F. and ZHONG, S. LAMBERT, S., MORRISON, J. and DEARING, S. A PIV investigation of the characteristics of micro-scale synthetic jets, pp Flow control with active dimples, pp 705-714. 509-518. LE MOIGNE, A., QIN, N. and WONG, W.S. HAGGERTY, A., MURMAN, E. and MCMANUS, H.L. Parallel adjoint-based optimisation of ab lended wing body aircraft with Lean engineering: a framework for doing the right thing right, pp 105-114. shock control bumps, pp 165-174. HARRIS, D. and LI, W.-C. LEONARDI, E., NEELY, A.J., DOIG, G. and BARBER, T.J. A systems approach to training aeronautical decision making: from The onset of compressibility effects for aerofoils in ground effect, Technical identifying training needs to verifying training solutions, pp 267-279. note, pp 797-806. HILLIER, R. and CREIGHTON, S. LESCHZINER, M.A. and LI, N. Experimental and computational study of unsteady hypersonic cavity Large-eddy simulation of separated flow over a swept wing with flows, pp 673-688. approximate near-wall modelling, pp 689-697. HILLS, N. LI, N. and LESCHZINER, M.A. Achieving high parallel performance for an unstructured unsteady Large-eddy simulation of separated flow over a swept wing with turbomachinery CFD code, pp 185-193. approximate near-wall modelling, pp 689-697. HOUWING, A.F.P., MCINTYRE, T.J. and KLEINE, H. LI, Q., PAGE, G.J. and MCGUIRK, J.J. Optical imaging techniques for hypersonic impulse facilities, pp 1-16. Large-eddy simulation of twin impinging jets in cross-flow, pp 195-206. HOWELL, R.J. and ROMAN, K.M. LI, W.-C. and HARRIS, D. Loss reduction on ultra high lift low-pressure turbine blades using A systems approach to training aeronautical decision making: from selective roughness and wake unsteadiness, pp 257-206. identifying training needs to verifying training solutions, pp 267-279. INDEX TO VOLUME 111 LIBRESCU, L., SONG, O. and KWON, H.D. NAYYAR, P., BARAKOS, G.N. and BADCOCK, K.J. Modelling and vibration of a non-classical tilt-rotor wing system, pp 285- Numerical study of transonic cavity flows using large-eddy and detached- 295. eddy simulation, pp 153-164. LOWENBERG, M., JONES, C., DUBS, A. and RICHARDSON, T. NEELY, A.J., DOIG, G., BARBER, T.J. and LEONARDI, E. Dynamic gain scheduled control of aH awk scale model, pp 461-469. The onset of compressibility effects for aerofoils in ground effect, Technical note, pp 797-806. MACPHERSON, A. and PRITCHARD, D. Strategic destruction of the Western commercial aircraft sector: NOBAHARI, H. and POURTAKDOUST, S.H. implications of system integration and international risk-sharing business An optimal-fuzzy two-phase CLOS guidance law design using ant colony models, pp 327-334. optimisation, pp 621-636. MAJUMDAR, A., TOUMI, R., OCHIENG, W., MOLLOY, J., NOLAND, R.B., MAJUMDAR, A., TOUMI, R., OCHIENG, W., WILLIAMS, V. and NOLAND, R.B. MOLLOY, J. and WILLIAMS, V. Reducing environmental! impacts of aviation with innovative air traffic Reducing environmental impacts of aviation with innovative air traffic management technologies, pp 741-749. management technologies, pp 741-749. MANESCHUJN, A., JONES, T., VON BACKSTROM, T.W. and OCHIENG, W., MOLLOY, J., WILLIAMS, V., NOLAND, R.B., INGHAM, L.A. MAJUMDAR, A. and TOUMIL, R. A proposed reference framework for unmanned aerial vehicle and system Reducing environmental impacts of aviation with innovative air traffic airworthiness requirements, pp 345-358. management technologies, pp 741-749. MANGLANO-VILLAMARIN, C.E. and SHAW, S.T. PACHIDIS, V., PILIDIS, P.,. MARINAI, L. and TEMPLALEXIS, I. Three-dimensional indicial response of finite aspect ratio yawed wings, pp Towards a full two dimensional gas turbine performance simulator, pp 359-371. 433-442. MANIMALA, B.J., WALKER, D.J., PADFIELD, G.D., VOSKUIJL, M. PADFIELD, G.D., VOSKUIJL, M., GUBBELS, A.W., MANIMALA, and GUBBELS, A.W. B.J. and WALKER, D.J. Rotorcraft simulation modelling and validation for control law design, pp Rotorcraft simulation modelling and validation for control law design, pp 77-88. 77-88. MARINAI, L., TEMPLALEXIS, I., PACHIDIS, V. and PILIDIS, P. PAGE, G.J., MCGUIRK, J.J. and LI, Q. Towards a full two dimensional gas turbine performance simulator, pp Large-eddy simulation of twin impinging jets in cross-flow, pp 195-206. 433-442. PASSMORE, M., RENDER, P. and JOHL, G. MCGUIRK, J.J., LI, Q. and PAGE, G.J. Design and performance of thin, circular arc, wind-tunnel turning vanes, Large-eddy simulation of twin impinging jets in cross-flow, pp 195-206. pp 115-118. MCINTYRE, T.J., KLEINE, H. and HOUWING, A.F.P. PEIRO, J.. CHANTHARASENAWONG, C. and GALVANETTO, U. Optical imaging techniques for hypersonic impulse facilities, pp 1-16. Remarks on the nonlinear dynamics of a typical aerofoil section in dynamic stall, pp 731-739. MCMANUS, H.L., HAGGERTY, A. and MURMAN, E. Lean engineering: a framework for doing the right thing right, pp 105-114. PERHINSCHI, M., CAMPA, G. and NAPOLITANO, MLR. Addressing pose estimation issues for machine vision based UAV MOLLOY, J., WILLIAMS, V., NOLAND, R.B., MAJUMDAR, A., autonomous aerial refuelling, pp 389-396. TOUMI, R. and OCHIENG, W. Reducing environmental impacts of aviation with innovative air traffic PERHINSCHI, M.G. and NAPOLITANO, MLR. management technologies, pp 741-749. Flight data reduction methodology for performance evaluation and comparison of model-following adaptive control laws, pp 807-814. MOORHOUSE, D., RIGGINS, D., TAYLOR, T. and TERHUNE, L. Methods for the design of energy efficient high-speed aerospace vehicles, PILIDIS, P., MARINAT, L., TEMPLALEXIS, I. AND PACHIDIS, V. pp 297-309. Towards a full two dimensionai gas turbine performance simulator, pp 433-442. MORRISON, J., DEARING, S. and LAMBERT, S. Flow control with active dimples, pp 705-714. PILIDIS, P.,. RAMSDEN, K. and KYRITSIS, V.E. The representation of GT component maps using Mach numbers, pp 453-460. MORTON, S.A., CUMMINGS, R.M., FORSYTHE, J.R. and WURTZLER, K. POURTAKDOUST, S.H. and NOBAHARI, H. High resolution computational unsteady aerodynamic techniques applied An optimal-fuzzy two-phase CLOS guidance law design using ant colony to maneouvering UCAVs, pp 397-404. optimisation, pp 621-636. MURMAN, E., MCMANUS, H.L. and HAGGERTY, A. PRICE, M., RAGHUNATHAN, S., BUTTERFIELD, J., GIBSON, A., Lean engineering: a framework for doing the right thing right, pp 105-114. CURRAN, R., CASTAGNE, S. and EARLY, J. Aircraft cost modelling using the genetic causal technique within a NADA, T.R. systems engineering approach, pp 409-420. Performance characterisation of MPD thrusters, pp 443-452. PRITCHARD, D. and MACPHERSON, A. NANGIA, R.K. Strategic Destruction of the Western commercial aircraft sector: ‘Greener’ civil aviation using air-to-air refuelling — relating aircraft design implications of system integration and international risk-sharing business efficiency and tanker offload efficiency, pp 589-592. models, pp 327-334. NAPOLITANO, M.R., PERHINSCHI, M. and CAMPA, G. PYLE, J.A., DESSENS, O. and ROGERS, H.L. Addressing pose estimation issues for machine vision based UAV A change in the calculated impact of supersonic aircraft NOx emissions on autonomous aerial refuelling, pp 389-396. the atmosphere, pp 311-314. NAPOLITANO, M.R. and PERHINSCHI, M.G. PYWELL, M. Flight data reduction methodology for performance evaluation and Developments in RF simulator technology — approaching the affordable comparison of model-following adaptive control laws, pp 807-814. limit, pp 545-560. THE AERONAUTICAL JOURNAL DECEMBER 2007 QIN, N., WONG, W.S. and LE MOIGNE, A. SHAW, S.T. and MANGLANO-VILLAMARIN, C.E. Parallel adjoint-based optimisation of a blended wing body aircraft with Three-dimensional indicial response of finite aspect ratio yawed wings, pp shock control bumps, pp 165-174. 359-371. RADESPIEL, R, YUAN, W., KHALID, M., WINDTE, J. and SCHOLZ, U. SHIVAKUMAR, K.N. and BHARGAVA, A. Computational and experimental investigations of low-Reynolds-number Three dimensional tensile stress concentration in countersunk, pp 777-786. flows past an aerofoil, pp 17-29. SINGH, S. and GHOSH, A.K. RADICE, G. and CASASCO, M. Estimation of lateral-directional parameters using neural networks based On different parameterisation methods to analyse spacecraft attitude modified delta method, pp 659-667. manoeuvres in the presence of attitude constrainsts, pp 335-342. SMART, M. RAGHUNATHAN, S., BUTTERFIELD, J., GIBSON, A., CURRAN, R., Scramjets, pp 605-619. CASTAGNE, S., EARLY, J. and PRICE, M. Aircraft cost modelling using the genetic causal technique within a SMITH, A.D., ELLIOTT, R., DI MARE, L. and IMREGUN, M. systems engineering approach, pp 409-420. A numerical study of high pressure turbine forced response in the presence of damaged nozzle guide vanes, pp 751-757. RAMSDEN, K., KYRITSIS, V.E. and PILIDIS, P. The representation of GT component maps using Mach numbers, pp 453-460. SMITH, H. A review of supersonic businesjse t design issues, pp 761-776. RASI MARZABADI, F. and SOLTANI, MLR. Effect of plunging amplitude on the performance of a wind turbine blade SOLTANI, M.R. and RASI MARZABADL, F. section, pp 571-587. Effect of plunging amplitude on the performance of a wind turbine blade section, pp 571-587. RASUO, B. Some analytical and numerical solutions for the safe turn manoeuvres of SONG, O., KWON, H.D. and LIBRESCU, L. agricultural aircraft — an overview, pp 593-599. Modelling and vibration of an on-classical tilt-rotor wing system, pp 285-295. REED, S.C. STEVENS, J.R.A., BRODIN, G.J. and COOPER, J.A. Development ofa parametric-based indirect aircraft structural usage Measuring the effect of helicopter rotors on GPS reception, pp 561-570. monitoring system using artificial neural networks, pp 209-230. SUNDERLAND, A.G., JOHNSTONE, R. and ALLEN, C.B. RENDER, P., JOHL, G. and PASSMORE, M. Application of a parallel rotor CFD code on HPCx, pp 145-152. Design and performance of thin, circular arc, wind-tunnel turning vanes, pp 115-118. SUNDERLAND, A.J., ASHWORTH, M., BADCOCK, K.J. and EMERSON, D.R. RICHARDSON, G.A., DAWES, W.N. and SAVILL, A.M. High performance computing and computational aerodynamics in the UK, An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion pp 125-131. control analysis, pp 133-144. TANG, H. and ZHONG, S. RICHARDSON, T., LOWENBERG, M., JONES, C. and DUBS, A. A static compressible flow model of synthetic jet actuators, pp 421-431. Dynamic gain scheduled control of aH awk scale model, pp 461-469. TANRIOVER, H. and SENOCAK, E. RIGGINS, D., TAYLOR, T., TERHUNE, L. and MOORHOUSE, D. Analysis of composite plates with variable stiffness using Galerkin Methods for the design of energy efficient high-speed aerospace vehicles, Method, pp 247-255. pp 297-309. TAO, C., DAREN, Y. and WEN, B. ROGERS, H.L., PYLE, J.A. and DESSENS, O. An idea of distributed parameter control for scramjet engines, pp 787-796. A change in the calculated impact of supersonic aircraft NOx emissions on the atmosphere, pp 311-314. TAYLOR, T., TERHUNE, L., MOORHOUSE, D. and RIGGINS, D. Methods for the design of energy efficient high-speed aerospace vehicles, ROMAN, K.M. and HOWELL, R.J. pp 297-309. Loss reduction on ultra high lift low-pressure turbine blades using selective roughness and wake unsteadiness, pp 257-206. TEMPLALEXIS, I., PACHIDIS, V., PILIDIS, P. and MARINAI, L. Towards a full two dimensional gas turbine performance simulator, pp 433-442. ROTARU, M. and BOTEZ, R.M. Relationships between flying qualities and flight tests parameters for the TERHUNE, L., MOORHOUSE, D., RIGGINS, D. and TAYLOR, T. F/A-18 aircraft, pp 281-282. Methods for the design of energy efficient high-speed aerospace vehicles, pp 297-309. SAHA, S. and CHAKRABORTY, D. Numerical exploration of starting process in supersonic nozzle, pp 51-58. TOUMI, R., OCHIENG, W., MOLLOY, J., WILLIAMS, V., NOLAND, R.B. and MAJUMDAR, A. SAVILL, A.M., RICHARDSON, G.A. and DAWES, W.N. Reducing environmental impacts of aviation with innovative air traffic An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion management technologies, pp 741-749. ‘ control analysis, pp 133-144. VOERSMANN, P., GANGULLI, R., JEHNERT, B. and WOLFRAM, J. SAVILL, A.M., RICHARDSON, G.A. and DAWES, W.N. Survivability of helicopter with individual blade primary control failure, An unsteady, moving mesh CFD simulation for Harrier hot-gas ingestion pp 645-657. control analysis, pp 133-144. VON BACKSTROM, T.W., INGHAM, L.A., MANESCHIJN, A. and SCHOLZ, U., RADESPIEL, R., YUAN, W., KHALID, M. and JONES, T. WINDTE, J. A proposed reference framework for unmanned aerial vehicle and system Computational and experimental investigations of low-Reynolds-number airworthiness requirements, pp 345-358. flows past an aerofoil, pp 17-29. VOSKUIJL, M., GUBBELS, A.W., MANIMALA, B.J., WALKER, D.J. SENOCAK, E. and TANRIOVER, H. and PADFIELD, G.D. Analysis of composite plates with variable stiffness using Galerkin Rotorcraft simulation modelling and validation for control law design, pp Method, pp 247-255. 77-88. INDEX TO VOLUME 111 WALKER, D.J., PADFIELD, G.D., VOSKUIJL, M., GUBBELS, A.W. WU, W.H., WANG, J.J., HUANG, Y. and CHEN, D.H. and MANIMALA, B.J. Investigation on the aerodynamic performance on an ejection seat, pp 373- Rotorcraft simulation modelling and validation for control law design, pp 380. 77-88. WURTZLER, K., MORTON, S.A., CUMMINGS, R.M. and WANG, J.J., HUANG, Y., CHEN, D.H. and WU, W.H. FORSYTHE, J.R. Investigation on the aerodynamic performance on an ejection seat, pp 373-380. High resolution computational unsteady aerodynamic techniques applied to maneouvering UCAVs, pp 397-404. WATSON, M., JAWORSKI, A.J. and WOOD, N.J. Application of synthetijce ta ctuators for the modification of the YOUBI, Z. and T. ZEBBICHE characteristics of separated shear layers on slender wings, pp 519-529. Effect of stagnation temperature on supersonic flow parameters application for air in nozzles, pp 31-40. WEN, B., TAO, C. and DAREN, Y., YUAN, K. and CAO, Y. An idea ofd istributed parameter control for scramjet engines, pp 787-796. Aircraft flight characteristics in conditions of windshear and icing, pp 41- 49. WILLIAMS, V., NOLAND, R.B., MAJUMDAR, A., TOUML, R., OCHIENG, W. and MOLLOY, J. YUAN, W., KHALID, M., WINDTE, J., SCHOLZ, U. and Reducing environmental impacts of aviation with innovative air traffic RADESPIEL, R. management technologies, pp 741-749. Computational and experimental investigations of low-Reynolds-number flows past an aerofoil, pp 17-29. WINDTE, J., SCHOLZ, U., RADESPIEL, R, YUAN, W. and KHALID, M. Computational and experimental investigations of low-Reynolds-number ZEBBICHE, T. and YOUBI, Z. flows past an aerofoil, pp 17-29. Effect of stagnation temperature on supersonic flow parameters application for air in nozzles, pp 31-40. WOLFRAM, J., VOERSMANN, P., GANGULI, R. and JEHNERT, B. Survivability of helicopter with individual blade primary control failure, ZHONG, S. and GUO, F. pp 645-657. A PIV investigation of the characteristics of micro-scale synthetic jets, pp 509-518. WONG, W.S., LE MOIGNE, A. and QIN, N. Parallel adjoint-based optimisation of a blended wing body aircraft with ZHONG, S. and TANG, H. shock control bumps, pp 165-174. A static compressible flow model of synthetijce t actuators, pp 421-431. WOOD, N.J., WATSON, M. and JAWORSKI, A.J. ZHU, G., BEARMAN, P.W. and GRAHAM, J.MLR. Application of syntheticje t actuators for the modification of the Prediction of drag and lift of wings from velocity and vorticity fields, pp characteristics of separated shear layers on slender wings, pp 519-529. 699-704. Volume CXI Number 1115 January pp 1-58 Number 1116 February pp 61-122 Number 1117 March pp 125-206 Number 1118 April pp 209-282 Number 1119 May pp 285-342 Number 1120 June pp 345-406 Number 1121 July pp 409-471 Number 1122 August pp 473-542 Number 1123 September pp 545-603 Number 1124 October pp 605-670 Number 1125 November pp 673-757 Number 1126 December pp 761-828

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