Table Of Content

[THE AERONAUTICAL JOURNAI DECEMBER 2002 THE AERONAUTICAL JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY Volume CVI January-December 2002 Subject Index ACOUSTICS echanism of windward vortex shocks about supersonic slender Active control of fan e trom high-bypass ratio ne yodies. S.A. Prince and N Qin, pp 507-519 experimental results. | ishardt. | Tapken, W P rT shock wave—turbulent boundary-layer interactions in the nann,p p 501-506 yresence of streamwise sloantd grsoove s. A.N. Smith, H Greener by desig tl echnology challenge. J.E. Gree ( I }.L. Fulker and P.R. Ashill. pp 193 500 of the nnology iI p 57-113 rical nul n of the vortex-fin interaction ove Hearing loss on the flight deck igin ¢ remedy B ive cylinder Omar. K. Chongman and R and M< 77-2 limising wing lift distribution to minimise wake vortex hazard AERODYNAMICS W.R. Graham, pp 413-426 A study of aerodynamic perfor degradation on aerof« ne Prediction of drag and lift using velocity and vorticity fields. G. Zhu, aircraft wings due to accreted ice. M. Khalid, F. ZI P.W. Bearman and J.M.R. Graham, pp 547-554. Chen, pp 461-472 Fechnical note. Near field study of vortex attenuation using wing-tip Aerodynamic performances of propellers with parametric lera blowing. R.G. Simpson, N.A. Ahmed and R.D. Archer,p p 117-120 tions on the optima! design. 5 Dd’ Angelo, | Berardi and I I S echnical note. The effect of a sequence of cavities on boundary pp 313-320 layer separation at M = 8-2. Z. He, J. Xiong, C. Lebas and J. Aerodynamics of delta wings with flaps at hypersonic sp tollery, pp 51-55 Ramesh, pp 293-312 he United Kingdom’s contributions to the development of aeronautics Autorotating rotor with ornithopter-like flapping blades. ‘ savor Part The development of the streamlined monoplane (the and M. Raikov, pp 399-409 920s-1940s). J.A.D. Ackroyd, pp 217-268. Causes for discrepancies in ground effect analyses. T.J. Barbet he use of pulse responses and system reduction for 2D unsteady Leonardi and D. Archer, pp 653-667 flows using the Euler equations. A.L. Gaitonde and D.P. Jones, pp Characterisation of wall flow topology in jet-in-crossflow interactio1 183-497 E.Y. Kwon and D. Chocinski, pp 393-398 lurbulence modelling and turbulent-flow computation in aeronautics Control of surface pressure fluctuations in reattaching flows by passive M.A. Leschziner and D. Drikakis, pp 349-384. means. R. Kumar and P.R. Viswanath,p p 669-674 steady aerodynamic calculations using three-dimensional Euler Experimental investigation of trailing-edge devices at transoni equations on unstructured dynamic grids. K.P. Sinhamahapatra, speeds. K. Richter and H. Rosemann, pp 185-193 pp 269-276 Flow visualisation of the orthogonal blade-vortex interaction using tilising CFD in the investigation of high-speed unsteady spiked particle image velocimetry. J.M. Early, R.B. Green an . body flows. D. Feszty, K.J. Badcock and B.E. Richards, pp 161- Coton, pp 137-145 174 Greener by design the technology challenge. J.E. Greet Wing aerodynamics and the science of compromise. Errata. J. Jupp, man of the Technology Sub-Group, pp 57-113. p55 Maximising the impact of CFD in the design office: ARA’s role A.J. Peace, pp 675-685 AEROELASTICITY Measurements of leading-edge vortices on a 75° delta planform wing \eroelastic computations using algebraic grid motion. C.B. Allen, at M = 2°5.1.M. Milanovic and I.M. Kalkhoran, pp 39-49 pp 559-570 [THE AERONAUTICAL JOURNAI DECEMBER 2002 THE AERONAUTICAL JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY Volume CVI January-December 2002 Subject Index ACOUSTICS echanism of windward vortex shocks about supersonic slender Active control of fan e trom high-bypass ratio ne yodies. S.A. Prince and N Qin, pp 507-519 experimental results. | ishardt. | Tapken, W P rT shock wave—turbulent boundary-layer interactions in the nann,p p 501-506 yresence of streamwise sloantd grsoove s. A.N. Smith, H Greener by desig tl echnology challenge. J.E. Gree ( I }.L. Fulker and P.R. Ashill. pp 193 500 of the nnology iI p 57-113 rical nul n of the vortex-fin interaction ove Hearing loss on the flight deck igin ¢ remedy B ive cylinder Omar. K. Chongman and R and M< 77-2 limising wing lift distribution to minimise wake vortex hazard AERODYNAMICS W.R. Graham, pp 413-426 A study of aerodynamic perfor degradation on aerof« ne Prediction of drag and lift using velocity and vorticity fields. G. Zhu, aircraft wings due to accreted ice. M. Khalid, F. ZI P.W. Bearman and J.M.R. Graham, pp 547-554. Chen, pp 461-472 Fechnical note. Near field study of vortex attenuation using wing-tip Aerodynamic performances of propellers with parametric lera blowing. R.G. Simpson, N.A. Ahmed and R.D. Archer,p p 117-120 tions on the optima! design. 5 Dd’ Angelo, | Berardi and I I S echnical note. The effect of a sequence of cavities on boundary pp 313-320 layer separation at M = 8-2. Z. He, J. Xiong, C. Lebas and J. Aerodynamics of delta wings with flaps at hypersonic sp tollery, pp 51-55 Ramesh, pp 293-312 he United Kingdom’s contributions to the development of aeronautics Autorotating rotor with ornithopter-like flapping blades. ‘ savor Part The development of the streamlined monoplane (the and M. Raikov, pp 399-409 920s-1940s). J.A.D. Ackroyd, pp 217-268. Causes for discrepancies in ground effect analyses. T.J. Barbet he use of pulse responses and system reduction for 2D unsteady Leonardi and D. Archer, pp 653-667 flows using the Euler equations. A.L. Gaitonde and D.P. Jones, pp Characterisation of wall flow topology in jet-in-crossflow interactio1 183-497 E.Y. Kwon and D. Chocinski, pp 393-398 lurbulence modelling and turbulent-flow computation in aeronautics Control of surface pressure fluctuations in reattaching flows by passive M.A. Leschziner and D. Drikakis, pp 349-384. means. R. Kumar and P.R. Viswanath,p p 669-674 steady aerodynamic calculations using three-dimensional Euler Experimental investigation of trailing-edge devices at transoni equations on unstructured dynamic grids. K.P. Sinhamahapatra, speeds. K. Richter and H. Rosemann, pp 185-193 pp 269-276 Flow visualisation of the orthogonal blade-vortex interaction using tilising CFD in the investigation of high-speed unsteady spiked particle image velocimetry. J.M. Early, R.B. Green an . body flows. D. Feszty, K.J. Badcock and B.E. Richards, pp 161- Coton, pp 137-145 174 Greener by design the technology challenge. J.E. Greet Wing aerodynamics and the science of compromise. Errata. J. Jupp, man of the Technology Sub-Group, pp 57-113. p55 Maximising the impact of CFD in the design office: ARA’s role A.J. Peace, pp 675-685 AEROELASTICITY Measurements of leading-edge vortices on a 75° delta planform wing \eroelastic computations using algebraic grid motion. C.B. Allen, at M = 2°5.1.M. Milanovic and I.M. Kalkhoran, pp 39-49 pp 559-570 INDEX TO VOLUME 106 687 \eroelasticity of two-dimensional lifting surfaces via indicial function Long, M.W. Radar reflectivity of land and sea Third Edition, approach. P. Marzocca, L. Librescu and G. Chiocchia, pp 147- p 146. Moore, F.G. Approximate methods for weapon aerodynamics Limit-cycle oscillation prediction for non-linear aeroelastic systems Progress in astronautics and aeronautics series, Volume 186, p 50 A. Sedaghat, J.E. Cooper, J.R. Wright and A.Y.T. Leung, pp 27- Niu, M.C.Y. Airframe stress analysis and sizing Second Edition, 32. p 50. Phe United Kingdom’s contributions to the development of aeronautics. Rahman, M. and Mulolani, 1. Applied vector analysis, p 291 Part 3. The development of the streamlined monoplane (the Saguat, P. Large eddy simulation for incompressible flows: an intro- 1920s-1940s). J.A.D. Ackroyd, pp 217-268. duction, p 146. rhe use of pulse responses and system reduction for 2D unsteady Serrano, S.E. Engineering uncertainty and risk analysis: a balanced flows using the Euler equations. A.L. Gaitonde and D.P. Jones, pp approach to probability, statistics, stochastic modelling, and 483-492. stochastic differential equations, p 146 Torsional/flexural response of large span wings to |l ig h altitude Simmons, F.S. Rocket exhaust plume phenomenology, p 410 turbulence. P.B.S. Lissaman and L.W. Brownlow, pp 32 5-335. Smetana, F.O. Flight vehicle performance and aerodynamic control, Unsteady aerodynamic calculations using three-dimensional Euler p 114. equations on unstructured dynamic grids. K.P. Sinhamahapatra, Stinton, D. The design of the aeroplane — Second Edition, p 459 pp 269-276. Vakin, S.A. et al Fundamentals of electronic warfare, p 583 Viot, A. Glare: history of the development of a new aircraft material, AEROSPACE ENGINEERING p 154. Velocity corrections in generalised Hohmann and bi-elliptic transfer Wirth, W.-D. Radar techniques using array antennas, p 627 orbits. O.M. Kamel and A.S. Soliman, pp 555-558 Yang et al Solid propellant chemistry, combustion, and motor interi- or ballistics. Progress in astronautics and aeronautics series, Volume AEROSPACE MEDICINE 185, p 410. Hearing loss on the flight deck origin and remedy. M. Bagshaw Yun, L. and Bliaut, A. Theory and design of air cushion craft, and M.C. Lower, pp 277-289. p 458. Human factors in multi-crew flight operations. H.W. Orlady and L.M. Orlady, pp 321-324. BOOK REVIEWS — BY TITLE Advanced mathematical methods in science and engineering. S.I AIRSHIPS Hayek, p 291. Linearised identification of the longitudinal flight dynamics of the Airframe stress analysis and sizing Second Edition. M.C.Y. Niu, solar powered airship Lotte. C.F. Eckersley and M.V. Cook, pp p 50. 571-581 Analysis of composite structures. C. Decolon, p 582 Applied CFD techniques: an introduction based on finite element BODIES methods. R. Lohner, p 458 Mechanism of windward vortex shocks about supersonic slender Applied vector analysis. M. Rahman and I. Mulolani, p 291 bodies. S.A. Prince and N. Qin, pp 507-519 Approximate methods for weapon aerodynamics. Progress in astro Numerical simulation of the vortex-fin interaction over a tangent- nautics and aeronautics series, Volume 186. F.G. Moore, p 50 ogive cylinder. A.A. Omar, K. Chongman and R. Oh-Hyun, pp ASM Handbook Volume 21 Composites. S.D. Henry et al (Eds), 175-184 p 582. Utilising CFD in the investigation of high-speed unsteady Boundary value problems for transonic flow. A.G. Kuz’min, p 627 spiked body flows. D. Feszty, KJ. Badcock and B.E. Richards, Building aerodynamics. T. Lawson, p 291 pp 161-174. Closure strategies for turbulent and transitional flows. B. Launder and N. Sandham (Eds), p 626 BOOK REVIEWS — BY AUTHOR Early developments of modern aerodynamics. J.A.D. Ackroyd, B.P Ackroyd, J.A.D., Axcell, B.P. and Ruban, A.1. Early developments Axcell and A.I. Ruban, p 202 of modern aerodynamics, p 202. Engineering uncertainty and risk analysis: a balanced approach to \liabadi, M.H. (Ed) Non-linear fracture and damage mechanisms, probability, statistics, stochastic modelling, and stochastic differ- pll4 ential equations. S.E. Serrano, p 146 Brooks, C.R. and Choudhury, A. Failure analysis of engineering Failure analysis of engineering materials. C.R. Brooks and A materials, p 194. Choudhury, p 194. Decolon, C. Analysis of composite structures, p 582 Flight vehicle performance and aerodynamic control. F.O. Smetana, Elishakoff, I. et al (Eds) Non-classical problems in the theory of p 114. elastic stability, p 626. Fundamentals of electronic warfare. S.A. Vakin et al, p 583 Fleeman, E.L. Tactical missile design, p 115. Glare: history of the development of a new aircraft material. A. Vlot, Hayek, S.1. Advanced mathematical methods in science and engineering, p 154. p 291. Gossamer spacecraft: membrane and inflatable structures technology Henry, S.D. et al (Eds) ASM Handbook Volume 21 Composites, for space applications. Progress in astronautics and aeronautics p 582 series, Volume 191.C.H.M. Jenkins (Ed), p 194. Jenkins, C.H.M. (Ed) Gossamer spacecraft: membrane and inflatable Large eddy simulation for incompressible flows: an introduction. P structures technology for space applications. Progress in astronautics Saguat, p 146. and aeronautics series, Volume 191, p 194. Non-classical problems in the theory of elastic stability. 1. Elishakoft Kuz’min, A.G. Boundary value problems for transonic flow, p 627. et al (Eds), p 626 Launder, B. and Sandham, N. (Eds) Closure strategies for turbulent Non-linear fracture and damage mechanisms. M.H. Aliabadi (Ed), p and transitional flows, p 626. 114. Lawson, T. Building aerodynamics, p 291. Physics of direct hit and near miss warhead technology. Progress Lloyd, R.M. Physics of direct hit and near miss warhead technology astronautics and aeronautics series, Volume 194. R.M. Lloyd, Progress in astronautics and aeronautics series, Volume 194, p 202. 202. Lohner, R. Applied CFD techniques: an introduction based on finite Radar reflectivity of land and sea — Third Edition. M.W. Long, element methods, p 458. 146. rICAL JOURNAI DECEMBER 2002 tray antennas. W.-D. Wirt rhe origins of greener by design. K. Mans and D. Marshall, p 57 nomenology. F.S. Simmot lhe United Kingdom’s contributions to the development of aeronautics istry, combustion, and moto! Part 3. The development of the streamlined monoplane (the utics and aeronautics series, \ 1920s-1940s). J.A.D. Ackroyd, pp 217-268 E.L. Fleeman, p 115 DYNAMICS oplane Second Edition. D. Stinton, j5 459 Advanced combat aircraft performance assessment. A. Kutschera of air cushion craft. L. Yun and A. Bliaut and P.M. Render, pp 443-451 Fuzzy logic approach for estimation of longitudinal aircraft parameters. M.S. Yaacob, H. Jamaluddin and K.C. Wong, pp 585-594 COMPOSITES Linearised identification of the longitudinal flight dynamics of the on S DUCKI " ng performance of anti-symn solar powered airship Lotte. C.F. Eckersley and M.V. Cook, pp effect on behaviour of membr 571-581 . pp 595-605 Modelling of the hose and drogue in air-to-air refuelling. A.W. Bloy and M.M. Khan, pp 17-26. COMPUTATIONAL FLUID DYNAMICS The United Kingdom’s contributions to the development of aeronautics Maximising the impact of CFD in the design Part 3. The development of the streamlined monoplane (the \.J. Peace, pp 1920s-1940s). J.A.D. Ackroyd,p p 217-268 Mechanism of windward vortex shocks about Torsional/flexural response of large span wings to high altitude bodies. S.A. Prince and N. Qin,p p 507-519 turbulence. P.B.S. Lissaman and L.W. Brownlow, pp 325-335 Numerical modelling of mixing in jets from castel vles and R.Y.T. Wong, py ENVIRONMENTAL ENGINEERING transition boundary-lay Greene! by design the technology challenge. J.E. Green, Chairman equation. M.G. Higazy, pp of the Technology Sub-Group, pp 57-113 the vortex-fin interactior lhe impacts of aviation on the atmosphere. H.L. Rogers, D.S. Lee, Omar, K. Chongman and D.W. Raper, P.M. de F. Foster, C.W. Wilson and P.J. Newton, pp 521-546 and lift using velocity and vorticity field Zhu id J.M.R. Graham, pp 547-554 FLUID MECHANICS nology for global flow inst ind control Characterisation of wall flow topology in jet-in-crossflow interaction ley and S. Sherwin, pp 61‘ E.Y. Kwon and D. Chocinski, pp 393-398 esponses and system reduction Control of surface pressure fluctuations in reattaching flows by passive ] ler equations. A.L. Gaitonde means. R. Kumar and P.R. Viswanath, pp 669-674 Numerical modelling of mixing in jets from castellated nozzles. AJ and turbulent-flow computat Saddington, K. Knowles and R.Y.T. Wong, pp 643-652 d D. Drikakis, pp 349-384 Numerical prediction of transition boundary-layer flows using new c calculations using three intermittency transport equation. M.G. Higazy, pp 337-347 ructured dynamic grids. K.P Spectral/hp element technology for global flow instability and control V. Theofilis, D. Barkley and S. Sherwin, pp 619-625 nvestigation of high-spee K J Badcock and B.I GUIDANCE AND NAVIGATION Control techniques for autonomous launching of ship-based unmanned air vehicles (UAVs). M.R. Crump and C. Bil, pp 121 COMPUTATIONAL TECHNIQUES (GENERAL) 128 elastic computations using algebraic grid 3 HISTORY t of exit separation on aircraft The United Kingdom’s contributions to the development of aeronautics O-second certification trials Part 3. The development of the streamlined monoplane (the ues. S.J 3lake, E.R. Gale 1920s-1940s). J.A.D. Ackroppy 21d7-,26 8 illippidis, pp 1-16 ch for estimation of longitudina HYPERSONIC FLOW Jamaluddin and K.C. Wong \erodynamics of delta wings with flaps at hypersonic speeds. R ent methodology and mode Ramesh, pp 293-312 L. Walls and J. Jones. pp Pec hnical n The effecto f sequence of cavities on boundary mpressive buckling performance of anti layer separation at M = 8-2. Z. He, J. Xiong, ¢ Lebas and J.l 1e effect on behaviour of membrar ral couplit Stollery, pp 51-55 ougnian, pp 595-605 Utilising CFD in the investigation of high-speed unsteady spiked body flows. D. Feszty, K.J. Badcock and B.E. Richards, DEFENCE pp 161-174 Integrated review of stealth technology and its ro Rao and S. P. Mahulikar, pp 629-641 ICING The NREL micro tactical expendable (MITE) ait \ study of aerodynamic performance degradation on aerofoils and C. Bovais, R. Foch, H. McFarlane, C. Sullir Dahlburg, aircraft wings due to accreted ice. M. Khalid, F. Zhang and S Gardner and R. Ramamurti, pp 431-441 Chen, pp 461-472 LIFTING SURFACES Air travel — greener by design. J.L.Stollery, p 57 \ study of aerodynamic performance degradation on aerofoils and Greener by design — the technology challenge. J.E. Green, Chairman aircraft wings due to accreted ice. M. Khalid, F. Zhang and S. of the Technology Sub-Group, pp 57-113 Chen, pp 461-472 INDEX TO VOLUME 106 Aerodynamics of delta wings with flaps at hypersonic speeds. R. RELIABILITY Ramesh, pp 293-312. Reliability enhancement methodology and modelling the REMM Aeroelastic computations using algebraic grid motion. C.B. Allen, project. J. Marshall, L.W alls and J. Jones, pp 195-201 pp 559-570. Aeroelasticity of two-dimensional lifting surfaces via indicial function REMOTELY PILOTED VEHICLES (RPVs) approach. P. Marzocca, L. Librescu and G. Chiocchia, pp 147- Control techniques for autonomous launching of ship-based 153. unmanned air vehicles (UAVs). M.R. Crump and C. Bil, pp 121-128. Causes for discrepancies in ground effect analyses. TJ. Barber, E. Leonardi and D. Archer, pp 653-667. SAFETY Experimental investigation of trailing-edge devices at transonic A study of aerodynamic performance degradation on aerofoils and speeds. K. Richter and H. Rosemann, pp 185-193. aircraft wings due to accreted ice. M. Khalid, F. Zhang and S$ Measurements of leading-edge vortices on a 75° delta planform wing Chen, pp 461-472. at M = 2:5. 1.M. Milanovic and I.M. Kalkhoran, pp 39-49. Examining the effect of exit separation on aircraft evacuation perfor- Optimising wing lift distribution to minimise wake vortex hazard. mance during 90-second certification trials using evacuation W.R. Graham, pp 413-426. modelling techniques. SJ. Blake, E.R. Galea, S. Gwynne, PJ Prediction of drag and lift using velocity and vorticity fields. G. Zhu, Lawrence and L. Fillippidis, pp 1-16 P.W. Bearman and J.M.R. Graham, pp 547-554. Future air traffic management passing the key tests. P. Brooker, The use of pulse responses and system reduction for 2D unsteady pp 211-215. flows using the Euler equations. A.L. Gaitonde and D.P. Jones, pp Human factors in multi-crew flight operations. H.W. Orlady and 483-492. L.M. Orlady, pp 321-324. Torsional/flexural response of large span wings to high altitude The case for flight simulation in general aviation. DJ. Allerton, pp turbulence. P.B.S. Lissaman and L.W. Brownlow, pp 3 25-335. 607-612. Turbulence modelling and turbulent-flow computation in aeronautics. The perceived gap between need(ed) and mandated training “mind M.A. Leschziner and D. Drikakis, pp 349-384. the gap”. P.G. Richards, pp 427-430 Unsteady aerodynamic calculations using three-dimensional Euler equations on unstructured dynamic grids. K.P. Sinhamahapatra, SHOCK WAVES pp 269-276. Mechanism of windward vortex shocks about supersonic slender Wing aerodynamics and the science of compromise. Errata. J. Jupp, bodies. S.A. Prince and N. Qin, pp 507-519. p>. Normal shock wave-turbulent boundary-layer interactions in the presence of streamwise slots and grooves. A.N. Smith, H. Babinsky, MAN-POWERED FLIGHT J.L. Fulker and P.R. Ashill, pp 493-500. The human-powered helicopter. A. Filippone, pp 613-618. Aircrew mission training via distributed simulation the potential MATERIALS in NATO. B. Tomlinson, pp 155-159. Micro-foamed structural materials for micro-aircraft. E. O°’K eefe, M. Examining the effect of exit separation on aircraft evacuation perfor Swan, R. Jones, V.G ergly and N. Cameron, pp 385-392. mance during 90-second certification trials using evacuation mod- elling techniques. SJ. Blake, E.R. Galea, S. Gwynne, PJ. METEOROLOGY Lawrence and L. Fillippidis, pp 1-16 Greener by design — the technology challenge. J.E. Green, Chairman Modelling of the hose and drogue in air-to-air refuelling. A.W. Bloy of the Technology Sub-Group, pp 57-113 and M.M. Khan, pp 17-26. The impacts of aviation on the atmosphere. H.L. Rogers, D.S. Lee, Simulation and collective training creating a total experience. E D.W. Raper, P.M. de F. Foster, C.W. Wilson and PJ. Newton, pp Smith and H.M. Mcintyre, pp 129-136 521-546. The case for flight simulation in general aviation. DJ. Allerton, pp 607-612 PROPULSION Active control of fan noise from high-bypass ratio aeroengines: STRENGTH ANALYSIS experimental results. L. Enghardt, U. Tapken, W. Neise. P The compressive buckling performance of anti-symmetric composite Schimming, R. Maier and J. Zillmann, pp 501-506. laminates and the effect on behaviour of membrane-flexural Aerodynamic performances of propellers with parametric considerations coupling. J. Loughlan, pp 595-605 on the optimal design. S. D’Angelo, F. Berardi and E. Minisci, pp The United Kingdom’s contributions to the development of aeronautics 313-320. Part 3. The development of the streamlined monoplane (the Greener by design — the technology challenge. J.E. Green, Chairman 1920s-1940s). J.A.D. Ackroyd,p p 217-268 of the Technology Sub-Group, pp 57-113 Integrated engine management: a new approach to health monitoring TESTING FACILITIES AND TECHNIQUES and control of gas turbine aero-engines. JJ. Gribble and G.J. Effect of tracer particle characteristics on visualisation of delta wing Dadd, pp 203-209. vortices. D.1. Greenwell, pp 473-482 Letter. R. FitzPatrick, p 215. Fuzzy logic approach for estimation of longitudinal aircraft parameters Maximising the impact of CFD in the design office: ARA’s role. M.S. Yaacob, H. Jamaluddin and K.C. Wong, pp 585-594 A.J. Peace, pp 675-685. Integrated engine management: a new approach to health monitoring Numerical modelling of mixing in jets from castellated nozzles. AJ. and control of gas turbine aero-engines. J.J. Gribble and GJ Saddington, K. Knowles and R.Y.T. Wong, pp 643-652. Dadd, pp 203-209 The impacts of aviation on the atmosphere. H.L. Rogers, D.S. Lee, Surface thermometry by laser-induced fluorescence of Dy**:YAG D.W. Raper, P.M. deF. Foster, C.W. Wilson and P.J. Newton, pp K. Kontis, Y. Syogenji and N. Yoshikawa, pp 453-457 521-548. The United Kingdom's contributions to the development of aeronautics. TRAINING Part 3. The development of the streamlined monoplane (the Aircrew mission training via distributed simulation the potential 1920s-1940s). J.A.D. Ackroyd, pp 217-268. in NATO, B. Tomlinson, pp 155-159 690 THE AERONAUTICAL JOURNAI DECEMBER 2002 Simulation and collective training creating a total experience. | Unsteady aerodynamic calculations using three-dimensional Euler Smith and H.M. McIntyre, pp 129-136. equations on unstructured dynamic grids. K.P. Sinhamahapatra The case for flight simulation in general aviation. DJ. Allerton, pp pp 269-276 Utilising CFD in the investigation of high-speed unsteady spiked between need(ed) and mandated training “mind body flows. D. Feszty, K.J. Badcock and B.E. Richards, pp 161-174 ichards, pp 427-430 V/STOL \utorotating rotor with ornithopter-like flapping blades. V. Savoy TRIBUTE and M. Raikov, pp 399-409 Dawn Steele, p 336 Flow visualisation of the orthogonal blade-vortex interaction using particle image velocimetry. J.M. Early, R.B. Green and F.N UNSTEADY AERODYNAMICS omg CoOnNtTrO!o l ¢ of surface iporieasmsauier e esc fluctuations in reatta‘cih ing flows by7 % passive lhe h; uman-powered helicopter. A. Filippone, pp 613S-6a1 8 sans. R. Kumar and P.R. Viswanath, pp 669-67 liltrotor development to meet public acceptability targe Spectral/hp element technology for global flow instability and control \ V. Theofilis, D. Bark4l5 ey and S.a ieS herwin, pp 619-625- Reber, pp 33-38 rhe use of pul esponses and system reduction for 2D unsteady WAKES flows using the Euler equations. A.L. Gaitonde and D1 ». Jones, pp Technical note. Near field study of vortex attenuation using wing-tip 183-497 blowing. R.G. Simpson, N.A. Ahmed and R.D. Archer, pp 117-120 lurbulence modelling and turbulent-flow computation in aeronautics Optimising wing lift distribution to minimise wake vortex M.A. Leschziner and D. Drikakis, pp 349-384 W.R. Graham, pp 413-426 Author Index ACKROYD, J.A.D. BEARMAN, P.W., ZHU, G. and GRAHAM, J.M.R. lhe United Kingdom's contributions to the development of aeronautic Prediction of drag and lift using velocity and vorticity field Part 3. The development of the streamlin yplane (th 554 ) 1-268 BERARDI,F ., D ANGELO, S. and MINISCI, E. AHME D, N.A., SIMPSON, R.G. and ARCHER, R.D. \erodynamic performanceso f propellersw i Near field study of vortex attenuat ° Wing-tip on the optin 313-3 BIL, C. and CRUMP, MLR. ALLEN, C.B. Control technique r autonomous Aeroelastic computati using algebri rid mot pp 559-570 unmanned air vel S AVs). pp 12 ALLERTON, D.J. BLAKE, S.J., GALEA, E.R., GWYNNS.E, ,LA WRENCE, The case for flight s lation in general aviatio | and FILLIPIDIS, L. ct of exit separation on all ARCHER, D., BARBER, T.J. and LEONARDI , ance during 90-second certification Causes for discrepancies in ground effect analys ( 667 modelling techniques,p p | ARCHER, R.D., SIMPSON, R.G. and AHMED, N.A. BLOY, A.W. and KHAN, M.M. Technical note. Near field study of vortex attent I ng-tip Modelling of the hose and dri BOVAIS, C., KELLOGG,J ., FOCR.H, M,cFA RLANE, ASHILL, P.R., SMITH, . BABINSKY, H. and FULKER, _ SULLIVAN, C., DAHLBURG, J., GARDNER, J. and Normal shock vave-ti storied boundar y-layer sint RAMAMURTI,.R presence of streamwise slots and grooves, pp 493 The NRL micro tactical expendable (MITE BABINSH.K, SYMI,TH , A.N., FULKER, J.L. and ASHILL, P.R. BROOKER, P. Normal shock wave-turbulent boundary-layer interactions in th Future air traf presenceo f streamwise slots and grooves, pp 49 BROWNLOW, L.W. and LISSAMAN, P.B.S. BADCOCK, K.J., FESZTY, D. and RICHARDSB,.E . ee ee ae ee eee ee ee Utilising CFD in the investigation of high-sp re body flows.p p 161-174 cial CAMERON, N., O’KEEFE, E., SWAN, M., JONESR., an d ‘ ; ' GERGLY,V . BAGSHAW, M. and LOWER, M.C. ; Micro-foamed structural materialsfo r micro-aircraft,p p 385 Hearing loss on the flight deck origin and 1 CHEN,S., KHALID, M. and ZHANG, F. BARBER, T.J., LEONARDI, E. and ARCHER, D \ study of aerodynamic performance degradation on aerofoils and Causes for discrepancies in ground effect analyses aircraft wings due to accreted ice, pp 461-472 BARKLEY, D., THEOFILIS, V. and SHERWIN, S. CHIOCCHIA, G., MARZOCCA, P. and LIBRESCU, L. Spectral/hp element technology for global flow instability and control, Aeroelasticity of two-dimensional lifting surfaces via indicial function pp 619-625. approach, pp 147-153 INDEX TO VOLUME 106 CHOCINSKI, D. and KWON, E.Y. FITZPATRICK, R. Characterisation of wall flow topology in jet-in-crossflow interaction, Letter, p 215 pp 393-398. FOCH, R., KELLOGG, J., BOVAIS, C., McFARLANE, H., CHONGMAN, K., OMAR, A.A. and OH-HYUN, R. SULLIVAN, C., DAHLBURG, J., GARDNER, J. and Numerical simulation of the vortex-fin interaction over a tangent- RAMAMURTI,R. ogive cylinder, pp 175-184. The NRL micro tactical expendable (MITE) air vehicle, pp 431-441 COOK, M.V. and ECKERSLEY, C.F. FOSTER, P.M. de F., ROGERS, H.L., LEE, D.S., RAPER, D.W., Linearised identification of the longitudinal flight dynamics of the WILSON, C.W. and NEWTON, P.J. solar powered airship Lotte, pp 571-581 The impacts of aviation on the atmosphere, pp 521-546 COOPER, J.E., SEDAGHAT, A., WRIGHT, J.R. and LEUNG, FULKJ.EL.,R SM,ITH , A.N., BABINSKHY. ,an d ASHILL, P.R. AY... Normal shock wave-turbulent boundary-layer interactions in the Limit-cycle oscillation prediction for non-linear aeroelastic systems, presence of streamwise slots and grooves, pp 493-500 pp 27-32. GAITONDE, A.L. and JONES, D.P. COTON, F.N., EARLY, J.M. and GREEN, R.B. The use of pulse responses and system reduction for 2D unsteady Flow visualisation of the orthogonal blade-vortex interaction using flows using the Euler equations, pp 483-492 particle image velocimetry, pp 13 145 GALEA, E.R., BLAKE, S.J., GWYNNE, S., LAWRENCE, PJ. CRUMP, M.R. and BIL, C. and FILLIPIDIS, L. Control techniques for autonomous launching of ship-based Examining the effect of exit separation on aircraft evacuation perfor unmanned air vehicles (UAVs), pp 121-128 mance during 90-second certification trials using evacuation mod elling techniques, pp 1-16 DADD, G.J. and GRIBBLE, J.J. Integrated engine management: a new approach to health monitoring GARDNER,J .,K ELLOGG, J., BOVAIS, C., FOCH, R., and control of gas turbine aero-engines, pp 203-209 McFARLANE, H., SULLIVAN, C., DAHLBURG,J . and RAMAMURTI, R. DAHLBURG,J ., KELLOGG,J ., BOVAIS, C., FOCH, R., The NRL micro tactical expendable (MITE) air vehicle, pp 431-441 McFARLANE, H., SULLIVAN, C., GARDNER, J. and RAMAMURTI,R. GERGLY, V., O°KEEFE, E., SWAN, M., JONES, R. and lhe NRL micro tactical expendable (MITE) air vehicle, pp 431-441. CAMERON,N. Micro-foamed structural materials for micro-aircraft, pp 385-392 D’ ANGELO, S., BERARDI, F. and MINISCI, E. \erodynamic performances of propellers with parametric considerations GRAHAM, J.M.R., ZHU, G. and BEARMAN, P.W, on the optimal design, pp 313-320 Prediction of drag and lift using velocity and vorticity fields, pp 547 554 DRIKAKIS, D. and LESCHZINER, M.A. lurbulence modelling and turbulent-flow computation in aeronau GRAHAM, W.R. tics, pp 349-384 Optimising wing lift distribution to minimise wake vortex hazard, pp 413-426 EARLY, J.M., GREEN, R.B. and COTON, F.N. Flow visualisation of the orthogonal blade-vortex interaction using GREEN, J.E. (Chairman of the Technology Sub-Group) particle image velocimetry, pp 137-145 Greener by design — the technology challenge, pp 57-113 ECKERSLEY, C.F. and COOK, M.YV. GREEN, R.B., EARLY, J.M. and COTON, F.N. Linearised identification of the longitudinal flight dynamics of the Flow visualisation of the orthogonal blade-vortex interaction using solar powered airship Lotte, pp 571-581 particle image velocimetry, pp 137-145 ENGHARDT, L., TAPKEN, U., NEISE, W., SCHIMMING, P., GREENWELL, D.1. MAIER, R. and ZILLMANN, J. Effect of tracer particle characteristics on visualisation of delta wing Active control of fan noise from high-bypass ratio aeroengines: ex vortices, pp 473-482 perimental results, pp 501-506 GRIBBLE, J.J. and DADD, G.J. FESZTY, D., BADCOCK, K.J. and RICHARDS, B.E. Integrated engine management: a new approach to health monitoring Utilising CFD in the investigation of high-speed unsteady spiked and control of gas turbine aero-engines, pp 203-209 body flows, pp 161-174. GWYNNE, S., BLAKE, S.J., GALEA, E.R., LAWRENCE, P.J. FILIPPONE,A . and FILLIPIDIS, L. lhe human-powered helicopter, pp 613-618 Examining the effect of exit separation on aircraft evacuation pertfor- mance during 90-second certification trials using evacuation mod- FILLIPIDIS, L., BLAKE, S.J., GALEA, E.R., GWYNNE, S. and elling techniques, pp 1-16 LAWRENCE, P.J. Examining the effect of exit separation on aircraft evacuation perfor- HE, Z., XIONG, J., LEBAS, C. and STOLLERY, J.L. mance during 90-second certification trials using evacuation Technical note. The effect of a sequence of cavities on boundary- modelling techniques, pp 1-16 layer separation at M = 8-2, pp 51-55. [THE AERONAUTICAL JOURNAI DECEMBER 2002 HIGAZY, M.G. LEBAS, C., HE, Z., XIONG,J .a nd STOLLERY, J.L. | pred f transition boundary-layer f Technical note. The effect of a sequence of cavities on boundary- pt ort equation, pp 337-347 layer separation at M = 8-2, pp 51-55 JAMALUDDIN, H., YAACOB, M.S. and WONG, K.C. LEE, D.S., ROGERS, H.L., RAPER, D.W., FOSTER, P.M. de ic approach for estimation of longitudinal air F., WILSON, C.W. and NEWTON, P.J. The impacts of aviation on the atmosphere, pp 521-546 .and GAITONDE, A LEONARDI, E., BARBER, T.J. and ARCHER, D. responses and system reductio1 Causes for discrepancies in ground effect analyses, pp 653-667 r equations, pp 483-492 LESCHZINER, M.A. and DRIKAKIS, D. .J.. MARSHALL, J. and WALLS, L. Turbulence modelling and turbulent-flow computation in aeronautics, ity enhancement methodology and modelli the REMM pp 349-384 n LEUNG, A.Y.T., SEDAGHAT, A., COOPER, J.E. and JONES, R., O°KEEFE, E., SWAN, M., GERGLY, V. and WRIGHT, J.R CAMERON,N . Limit-cycle oscillation prediction for non-linear aeroelastic systems Micro-toamed structur naterialsfo r micro-aircraft JUPP, J. LIBRESCU, L., MARZOCCA, P. and CHIOCCHIA, G. Wing aerodyna cS and the science of comprom Aeroelasticity of two-dimensional lifting surfaces via indicial function approach, pp 147-153 KALKHORAN, I.M. and MILANOVIC, I.M. Measurements « eading-edge vorticeosn a 75 LISSAMAN, P.B.S. and BROWNLOW, L.W. tM =2°5,1 orsional/flexural response of large span wings to high altitude turbulence KAMEL, O.M. and SOLIMAN, ASS. Velocity correction generalised Hohmann an LOUGHLAN, J. SS55_S58 Che compressive buckling performance of anti-symmetric composite linates and the effect behaviour of membrane-flexural KELLOGJG.,, B OVAIS, C., FOCHR.,, McFARLANE, H., coupling. pp 595-605 SULLIVAN, C., DAHLBURG, J., GARDNER, J. and RAMAMURTI,R. LOWER, M.C. and BAGSHAW, M. e NRL micro tactic il expendable (MITE ) all Hearing loss on the flight deck origin and remedy, pp 2 KHALID, M., ZHANG, F. and CHEN,S . McFARLANE, H., KELLOGG, J., BOVAIS, C., FOCH, R., \ study of ae nic performance degradat SULLIVAN, C., DAHLBURG, J., GARDNEJR. ,an d creted Ice pp 4“611 474% RAMAMURTI,R. he NRL micro tactical expendable (MITE) air vehicle, pp 431-441 KHAN, M.M. and BLOY, A.W. Modelling of the hose and drogue in air-to-au Mc:NHT.M.Y anRd SEMIT,H, E. Simulation and collective training | experience, pp KNOWLES, K., SADDINGTON, A.J. and WONG, R.Y. 129-136 Numerical modelli »f mixing in jets from cast ! (6 4 MAHULIKAR,S. P. and RAO, G.A. Integrated review of stealth technology and its role in airpowet KONTIS,K ., SYOGENJI, Y. and YOSHIKAWA, N. 629-64] by laser-induced fluores MAIER, R., ENGHARDT, L., TAPKEN, U., NEISE, W SCHIMP.M anId ZNILLGMAN,N, J. KUMAR, R. and VISWANATH, P.R. Active control of fan noise from high-bypass ratio aeroengines Control of surface pressure fluctuations in experimental results, pp 501-506 passive means, pp 669-674 MANS, K. and MARSHALL, D KI TOLEERA A, A. and RENDER, P.M. rhe origins of greener by design, p 57 Advanced combat aircraft performance assessme MARSHALL, D. and MANS, K. KWON, E.Y. and CHOCINSKI, D. rhe origins of greener by design, p 5 Characterisation of wall flow topology in jet-in-crossflow interaction pp 393-398 MARSHALL, J., WALLS, L. and JONES,J . Reliability enhancement methodology and modelling the REMM LAWRENCE, P.J., BLAKE, S.J., GALEA, E.R., GWYNNE, S project, pp 195-201 and FILLIPIDIS, L. Examining the effect of exit separation on aircraft evacuation perfor MARZOCCA, P., LIBRESCU, L. and CHIOCCHIA,G. mance during 90-second certification trials using evacuation Acroelasticity of two-dimensional lifting surfaces via indicial function modelling techniques, pp 1-16. approach, pp 147-153 INDEX TO VOLUME 106 MILANOVIC, I.M. and KALKHORAN, LM. RENDEP.RM., a nd KUTSCHERA, A. Measurements of leading-edge vortices on a 75° delta planform wing Advanced combat aircraft performance assessment, pp 443-451 at M = 2:5, pp 39-49. RICHARDS, B.E., FESZTY, D. and BADCOCK, K.J. MINISCI, E., DDANGELO, S. and BERARDI, F. Utilising CFD in the investigation of high-speed unsteady spiked Aerodynamic performances of propellers with parametric considerations body flows, pp 161-174 on the optimal design, pp 313-320 RICHARDS, P.G. NEISE, W., ENGHARDT, L., TAPKEN, U., SCHIMMING, P., The perceived gap between need(ed) and mandated training “mind MAIER, R. and ZILLMANN, J. the gap”, pp 427-430 Active control of fan noise from high-bypass ratio aeroengines experimental results, pp 501-506 RICHTER, K. and ROSEMANN, H. Experimental investigation of trailing-edge devices at transonic NEWTON, P.J., ROGERS, H.L., LEE, D.S., RAPER, D.W., speeds, pp 185-193 FOSTER, P.M. de F. and WILSON, C.W. Che impacts of aviation on the atmosphere, pp 521-546 ROGERS, H.L., LEE, D.S., RAPER, D.W., FOSTER, P.M. de OH-HYUN, R., OMAR, A.A. and CHONGMAN, K. F., WILSON, C.W. and NEWTON, P.J. Numerical simulation of the vortex-fin interaction over a tangent- The impacts of aviation on the atmosphere, pp 521-546 ogive cylinder, pp 175-184 ROSEMANN, H. and RICHTER, K. O°’ KEEFE, E., SWAN, M., JONES, R., GERGLY, V. and Experimental investigation of trailing-edge devices at transonic CAMERON,N. speeds, pp 185-193 Micro-foamed structural materials for micro-aircraft, pp 385-392 SADDINGTON, A.J., KNOWLES, K. and WONG, R.Y.T. OMAR, A.A., CHONGMAN, K. and OH-HYUN, R. Numerical modelling of mixing in jets from castellated nozzles, pp Numerical simulation of the vortex-fin interaction over a tangent 643-65? ogive cylinder, pp 175-184 SAVOV, V. and RAIKOV, M. ORLADY, H.W. and ORLADY, L.M. Autorotating rotor with ornithopter-like flapping blades, pp 399-409 Human factors in multi-crew flight operations, pp 321-324 SCHIMMING,P ., ENGHARDT, L., TAPKEN, U., NEISE, W., ORLADY, L.M. and ORLADY, H.W. MAIERR., a nd ZILLMANN, J. Human factors in multi-crew flight operations, pp 321-324 Active control of fan noise from high-bypass ratio aeroengines experimental results, pp 501-506 PEACE, A.J. Maximising the impact of CFD in the design office: ARA’s role., pp SEDAGHAT, A., COOPER, J.E., WRIGHT, J.R. and LEUNG, 675-685. Awe Limit-cycle oscillation prediction for non-linear aeroelastic systems, PRINCS.EA. ,a nd QIN, N. pp 27-32 Mechanism of windward vortex shocks about supersonic slendet bodies, pp 507-519 SHERWIN, S., THEOFILIS, V. and BARKLEY, D. Spectral/hp element technology for global flow instability and control QIN, N. and PRINCE, S.A. pp 619-625 Mechanism of windward vortex shocks about supersonic slender bodies, pp 507-519 SIMPSON, R.G., AHMED, N.A. and ARCHER, R.D. Technical note. Near field study of vortex attenuation using wing-tip RAIKOV, M. and SAVOV, V. blowing, pp 117-120 Autorotating rotor with ornithopter-like flapping blades, pp 399-409 SINHAMAHAPATRA, K.P. RAMAMURTI, R., KELLOGG, J., BOVAIS, C., FOCH, R., Unsteady aerodynamic calculations using three-dimensional Euler McFARLANE, H., SULLIVAN, C., DAHLBURG, J. and equations on unstructured dynamic grids, pp 269-276 GARDNER,J . The NRL micro tactical expendable (MITE) air vehicle, pp 431-441 SMITH, A.N., BABINSKY, H., FULKER, J.L. and ASHILL, PR. RAMESH,R . Normal shock wave-—turbulent boundary-layer interactions in the Aerodynamics of delta wings with flaps at hypersonic speeds, pp presence of streamwise slots and grooves, pp 493-500 293-312. RAO, G.A. and MAHULIKAR, S.P. SMITH, E. and McINTYRE, H.M. Integrated review of stealth technology and its role in airpower, pp Simulation and collective training creating a total experience, pp 629-641 129-136 RAPER, D.W., ROGERS, H.L., LEE, D.S., FOSTER, P.M. de SOLIMAN, A\S. and KAMEL, O.M. F., WILSON, C.W. and NEWTON, P.J. Velocity corrections in generalised Hohmann and bi-elliptic transfer The impacts of aviation on the atmosphere, pp 521-546 REBER, R.R. STOLLERY, J.L. Tiltrotor development to meet public acceptability targets, pp 33-38. Air travel — greener by design, p 57 694 THE AERONAUTICAL JOURNAI DECEMBER 2002 STOLLERY, J.L., HE, Z., XIONG,J . and LEBAS, C. WILSON, C.W., ROGERS, H.L., LEE, D.S., RAPER, D.W., fechnical note. The effect of a sequence of cavities on boundary- FOSTER, P.M. de F. and NEWTON, PJ. layer separation at M = 8-2, pp 51-55. The impacts of aviation on the atmosphere, pp 521-546 WONG, K.C., YAACOB, M.S. and JAMALUDDIN, H. SULLIVAN, C., KELLOGG, J., BOVAIS, C., FOCH, R., Fuzzy logic approach for estimation of longitudinal aircraft parameters, McFARLANE, H., DAHLBURG,J ., GARDNER, J. and pp 585-594 RAMAMURTI,R. The NRL micro tactical expendable (MITE) air vehicle, pp 431-441 WONG, R.Y.T., SADDINGTON, A.J. and KNOWLES, K. Numerical modelling of mixing in jets from castellated nozzles, pp SWAN, M., O’KEEFE, E., JONES, R., GERGLY, V. and 643-652 CAMERON,N. Micro-foamed structural materials for micro-aircraft, pp 385-392 WRIGHT, J.R., SEDAGHAT, A., COOPER, J.E. and LEUNG, A.¥.i. SYOGENJI, Y., KONTIS, K. and YOSHIKAWA, N. Limit-cycle oscillation prediction for non-linear aeroelastic systems, Surface thermometry by laser-induced fluorescence of Dy*+:YAG, pp 27-32 pp 453-457 XIONG, J., HE, Z., LEBAS, C. and STOLLERY, J.L. Technical note. The effect of a sequence of cavities on boundary- TAPKEN, U., ENGHARDT, L., NEISE, W., SCHIMMING, P., layer separation at M = 8-2, pp 51-55. MAIER, R. and ZILLMANN,J . Active control of fan noise from high-bypass ratio aeroengines YAACOB, MSS., JAMALUDDIN, H. and WONG, K.C. experimental results, pp 501-506. Fuzzy logic approach for estimation of longitudinal aircraft parameters, pp 585-594 THEOFILIS, V., BARKLEY, D. and SHERWIN, S. Spectral/hp element technology for global flow instability and control, YOSHIKAWA, N., KONTIS, K. and SYOGENJI, Y. pp 619-625 Surface thermometry by laser-induced fluorescence of Dy*+:YAG, pp 453-457 TOMLINSON, B. ZHANG, F., KHALID, M. and CHEN, S. Aircrew mission training via distributed simulation the potential \ study of aerodynamic performance degradation on aerofoils and in NATO, pp 155-159 aircraft wings due to accreted ice, pp 461-472 VISWANATH, P.R. and KUMAR, R. ZHU, G., BEARMAN, P.W. and GRAHAM, J.M.R. Control of surface pressure fluctuations in reattaching Prediction of drag and lift using velocity and vorticity fields, pp 547-554 passive means, pp 669-674 ZILLMANN, J., ENGHARDT, L., TAPKEN, U., NEISE, W., WALLS, L., MARSHALL,J . and JONES,J . SCHIMMING, P. and MAIER, R. Reliability enhancement methodology and modelling the REMM Active control of fan noise from high-bypass ratio aeroengines project, pp 195-201 experimental results, pp 501-506 Volume CVI Number 1055 January pp 1-55 Number 1056 February pp 57-115 Number 1057 March pp 117-159 Number 1058 April pp 161-215 Number 1059 May pp 217-291 Number 1060 June pp 293-347 Number 1061 July pp 349-411 Number 1062 \ugust pp 413-459 Number 1063 September pp 461-519 Number 1064 October pp 521-583 Number 1065 November pp 585-627 Number 1066 December pp 629-695

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[THE AERONAUTICAL JOURNAI DECEMBER 2002 THE AERONAUTICAL JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY Volume CVI January-December 2002 Subject Index ACOUSTICS echanism of windward vortex shocks about supersonic slender Active control of fan e trom high-bypass ratio ne yodies. S.A. Prince and N Qin, pp 507-519 experimental results. | ishardt. | Tapken, W P rT shock wave—turbulent boundary-layer interactions in the nann,p p 501-506 yresence of streamwise sloantd grsoove s. A.N. Smith, H Greener by desig tl echnology challenge. J.E. Gree ( I }.L. Fulker and P.R. Ashill. pp 193 500 of the nnology iI p 57-113 rical nul n of the vortex-fin interaction ove Hearing loss on the flight deck igin ¢ remedy B ive cylinder Omar. K. Chongman and R and M< 77-2 limising wing lift distribution to minimise wake vortex hazard AERODYNAMICS W.R. Graham, pp 413-426 A study of aerodynamic perfor degradation on aerof« ne Prediction of drag and lift using velocity and vorticity fields. G. Zhu, aircraft wings due to accreted ice. M. Khalid, F. ZI P.W. Bearman and J.M.R. Graham, pp 547-554. Chen, pp 461-472 Fechnical note. Near field study of vortex attenuation using wing-tip Aerodynamic performances of propellers with parametric lera blowing. R.G. Simpson, N.A. Ahmed and R.D. Archer,p p 117-120 tions on the optima! design. 5 Dd’ Angelo, | Berardi and I I S echnical note. The effect of a sequence of cavities on boundary pp 313-320 layer separation at M = 8-2. Z. He, J. Xiong, C. Lebas and J. Aerodynamics of delta wings with flaps at hypersonic sp tollery, pp 51-55 Ramesh, pp 293-312 he United Kingdom’s contributions to the development of aeronautics Autorotating rotor with ornithopter-like flapping blades. ‘ savor Part The development of the streamlined monoplane (the and M. Raikov, pp 399-409 920s-1940s). J.A.D. Ackroyd, pp 217-268. Causes for discrepancies in ground effect analyses. T.J. Barbet he use of pulse responses and system reduction for 2D unsteady Leonardi and D. Archer, pp 653-667 flows using the Euler equations. A.L. Gaitonde and D.P. Jones, pp Characterisation of wall flow topology in jet-in-crossflow interactio1 183-497 E.Y. Kwon and D. Chocinski, pp 393-398 lurbulence modelling and turbulent-flow computation in aeronautics Control of surface pressure fluctuations in reattaching flows by passive M.A. Leschziner and D. Drikakis, pp 349-384. means. R. Kumar and P.R. Viswanath,p p 669-674 steady aerodynamic calculations using three-dimensional Euler Experimental investigation of trailing-edge devices at transoni equations on unstructured dynamic grids. K.P. Sinhamahapatra, speeds. K. Richter and H. Rosemann, pp 185-193 pp 269-276 Flow visualisation of the orthogonal blade-vortex interaction using tilising CFD in the investigation of high-speed unsteady spiked particle image velocimetry. J.M. Early, R.B. Green an . body flows. D. Feszty, K.J. Badcock and B.E. Richards, pp 161- Coton, pp 137-145 174 Greener by design the technology challenge. J.E. Greet Wing aerodynamics and the science of compromise. Errata. J. Jupp, man of the Technology Sub-Group, pp 57-113. p55 Maximising the impact of CFD in the design office: ARA’s role A.J. Peace, pp 675-685 AEROELASTICITY Measurements of leading-edge vortices on a 75° delta planform wing \eroelastic computations using algebraic grid motion. C.B. Allen, at M = 2°5.1.M. Milanovic and I.M. Kalkhoran, pp 39-49 pp 559-570 [THE AERONAUTICAL JOURNAI DECEMBER 2002 THE AERONAUTICAL JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY Volume CVI January-December 2002 Subject Index ACOUSTICS echanism of windward vortex shocks about supersonic slender Active control of fan e trom high-bypass ratio ne yodies. S.A. Prince and N Qin, pp 507-519 experimental results. | ishardt. | Tapken, W P rT shock wave—turbulent boundary-layer interactions in the nann,p p 501-506 yresence of streamwise sloantd grsoove s. A.N. Smith, H Greener by desig tl echnology challenge. J.E. Gree ( I }.L. Fulker and P.R. Ashill. pp 193 500 of the nnology iI p 57-113 rical nul n of the vortex-fin interaction ove Hearing loss on the flight deck igin ¢ remedy B ive cylinder Omar. K. Chongman and R and M< 77-2 limising wing lift distribution to minimise wake vortex hazard AERODYNAMICS W.R. Graham, pp 413-426 A study of aerodynamic perfor degradation on aerof« ne Prediction of drag and lift using velocity and vorticity fields. G. Zhu, aircraft wings due to accreted ice. M. Khalid, F. ZI P.W. Bearman and J.M.R. Graham, pp 547-554. Chen, pp 461-472 Fechnical note. Near field study of vortex attenuation using wing-tip Aerodynamic performances of propellers with parametric lera blowing. R.G. Simpson, N.A. Ahmed and R.D. Archer,p p 117-120 tions on the optima! design. 5 Dd’ Angelo, | Berardi and I I S echnical note. The effect of a sequence of cavities on boundary pp 313-320 layer separation at M = 8-2. Z. He, J. Xiong, C. Lebas and J. Aerodynamics of delta wings with flaps at hypersonic sp tollery, pp 51-55 Ramesh, pp 293-312 he United Kingdom’s contributions to the development of aeronautics Autorotating rotor with ornithopter-like flapping blades. ‘ savor Part The development of the streamlined monoplane (the and M. Raikov, pp 399-409 920s-1940s). J.A.D. Ackroyd, pp 217-268. Causes for discrepancies in ground effect analyses. T.J. Barbet he use of pulse responses and system reduction for 2D unsteady Leonardi and D. Archer, pp 653-667 flows using the Euler equations. A.L. Gaitonde and D.P. Jones, pp Characterisation of wall flow topology in jet-in-crossflow interactio1 183-497 E.Y. Kwon and D. Chocinski, pp 393-398 lurbulence modelling and turbulent-flow computation in aeronautics Control of surface pressure fluctuations in reattaching flows by passive M.A. Leschziner and D. Drikakis, pp 349-384. means. R. Kumar and P.R. Viswanath,p p 669-674 steady aerodynamic calculations using three-dimensional Euler Experimental investigation of trailing-edge devices at transoni equations on unstructured dynamic grids. K.P. Sinhamahapatra, speeds. K. Richter and H. Rosemann, pp 185-193 pp 269-276 Flow visualisation of the orthogonal blade-vortex interaction using tilising CFD in the investigation of high-speed unsteady spiked particle image velocimetry. J.M. Early, R.B. Green an . body flows. D. Feszty, K.J. Badcock and B.E. Richards, pp 161- Coton, pp 137-145 174 Greener by design the technology challenge. J.E. Greet Wing aerodynamics and the science of compromise. Errata. J. Jupp, man of the Technology Sub-Group, pp 57-113. p55 Maximising the impact of CFD in the design office: ARA’s role A.J. Peace, pp 675-685 AEROELASTICITY Measurements of leading-edge vortices on a 75° delta planform wing \eroelastic computations using algebraic grid motion. C.B. Allen, at M = 2°5.1.M. Milanovic and I.M. Kalkhoran, pp 39-49 pp 559-570 INDEX TO VOLUME 106 687 \eroelasticity of two-dimensional lifting surfaces via indicial function Long, M.W. Radar reflectivity of land and sea Third Edition, approach. P. Marzocca, L. Librescu and G. Chiocchia, pp 147- p 146. Moore, F.G. Approximate methods for weapon aerodynamics Limit-cycle oscillation prediction for non-linear aeroelastic systems Progress in astronautics and aeronautics series, Volume 186, p 50 A. Sedaghat, J.E. Cooper, J.R. Wright and A.Y.T. Leung, pp 27- Niu, M.C.Y. Airframe stress analysis and sizing Second Edition, 32. p 50. Phe United Kingdom’s contributions to the development of aeronautics. Rahman, M. and Mulolani, 1. Applied vector analysis, p 291 Part 3. The development of the streamlined monoplane (the Saguat, P. Large eddy simulation for incompressible flows: an intro- 1920s-1940s). J.A.D. Ackroyd, pp 217-268. duction, p 146. rhe use of pulse responses and system reduction for 2D unsteady Serrano, S.E. Engineering uncertainty and risk analysis: a balanced flows using the Euler equations. A.L. Gaitonde and D.P. Jones, pp approach to probability, statistics, stochastic modelling, and 483-492. stochastic differential equations, p 146 Torsional/flexural response of large span wings to |l ig h altitude Simmons, F.S. Rocket exhaust plume phenomenology, p 410 turbulence. P.B.S. Lissaman and L.W. Brownlow, pp 32 5-335. Smetana, F.O. Flight vehicle performance and aerodynamic control, Unsteady aerodynamic calculations using three-dimensional Euler p 114. equations on unstructured dynamic grids. K.P. Sinhamahapatra, Stinton, D. The design of the aeroplane — Second Edition, p 459 pp 269-276. Vakin, S.A. et al Fundamentals of electronic warfare, p 583 Viot, A. Glare: history of the development of a new aircraft material, AEROSPACE ENGINEERING p 154. Velocity corrections in generalised Hohmann and bi-elliptic transfer Wirth, W.-D. Radar techniques using array antennas, p 627 orbits. O.M. Kamel and A.S. Soliman, pp 555-558 Yang et al Solid propellant chemistry, combustion, and motor interi- or ballistics. Progress in astronautics and aeronautics series, Volume AEROSPACE MEDICINE 185, p 410. Hearing loss on the flight deck origin and remedy. M. Bagshaw Yun, L. and Bliaut, A. Theory and design of air cushion craft, and M.C. Lower, pp 277-289. p 458. Human factors in multi-crew flight operations. H.W. Orlady and L.M. Orlady, pp 321-324. BOOK REVIEWS — BY TITLE Advanced mathematical methods in science and engineering. S.I AIRSHIPS Hayek, p 291. Linearised identification of the longitudinal flight dynamics of the Airframe stress analysis and sizing Second Edition. M.C.Y. Niu, solar powered airship Lotte. C.F. Eckersley and M.V. Cook, pp p 50. 571-581 Analysis of composite structures. C. Decolon, p 582 Applied CFD techniques: an introduction based on finite element BODIES methods. R. Lohner, p 458 Mechanism of windward vortex shocks about supersonic slender Applied vector analysis. M. Rahman and I. Mulolani, p 291 bodies. S.A. Prince and N. Qin, pp 507-519 Approximate methods for weapon aerodynamics. Progress in astro Numerical simulation of the vortex-fin interaction over a tangent- nautics and aeronautics series, Volume 186. F.G. Moore, p 50 ogive cylinder. A.A. Omar, K. Chongman and R. Oh-Hyun, pp ASM Handbook Volume 21 Composites. S.D. Henry et al (Eds), 175-184 p 582. Utilising CFD in the investigation of high-speed unsteady Boundary value problems for transonic flow. A.G. Kuz’min, p 627 spiked body flows. D. Feszty, KJ. Badcock and B.E. Richards, Building aerodynamics. T. Lawson, p 291 pp 161-174. Closure strategies for turbulent and transitional flows. B. Launder and N. Sandham (Eds), p 626 BOOK REVIEWS — BY AUTHOR Early developments of modern aerodynamics. J.A.D. Ackroyd, B.P Ackroyd, J.A.D., Axcell, B.P. and Ruban, A.1. Early developments Axcell and A.I. Ruban, p 202 of modern aerodynamics, p 202. Engineering uncertainty and risk analysis: a balanced approach to \liabadi, M.H. (Ed) Non-linear fracture and damage mechanisms, probability, statistics, stochastic modelling, and stochastic differ- pll4 ential equations. S.E. Serrano, p 146 Brooks, C.R. and Choudhury, A. Failure analysis of engineering Failure analysis of engineering materials. C.R. Brooks and A materials, p 194. Choudhury, p 194. Decolon, C. Analysis of composite structures, p 582 Flight vehicle performance and aerodynamic control. F.O. Smetana, Elishakoff, I. et al (Eds) Non-classical problems in the theory of p 114. elastic stability, p 626. Fundamentals of electronic warfare. S.A. Vakin et al, p 583 Fleeman, E.L. Tactical missile design, p 115. Glare: history of the development of a new aircraft material. A. Vlot, Hayek, S.1. Advanced mathematical methods in science and engineering, p 154. p 291. Gossamer spacecraft: membrane and inflatable structures technology Henry, S.D. et al (Eds) ASM Handbook Volume 21 Composites, for space applications. Progress in astronautics and aeronautics p 582 series, Volume 191.C.H.M. Jenkins (Ed), p 194. Jenkins, C.H.M. (Ed) Gossamer spacecraft: membrane and inflatable Large eddy simulation for incompressible flows: an introduction. P structures technology for space applications. Progress in astronautics Saguat, p 146. and aeronautics series, Volume 191, p 194. Non-classical problems in the theory of elastic stability. 1. Elishakoft Kuz’min, A.G. Boundary value problems for transonic flow, p 627. et al (Eds), p 626 Launder, B. and Sandham, N. (Eds) Closure strategies for turbulent Non-linear fracture and damage mechanisms. M.H. Aliabadi (Ed), p and transitional flows, p 626. 114. Lawson, T. Building aerodynamics, p 291. Physics of direct hit and near miss warhead technology. Progress Lloyd, R.M. Physics of direct hit and near miss warhead technology astronautics and aeronautics series, Volume 194. R.M. Lloyd, Progress in astronautics and aeronautics series, Volume 194, p 202. 202. Lohner, R. Applied CFD techniques: an introduction based on finite Radar reflectivity of land and sea — Third Edition. M.W. Long, element methods, p 458. 146. rICAL JOURNAI DECEMBER 2002 tray antennas. W.-D. Wirt rhe origins of greener by design. K. Mans and D. Marshall, p 57 nomenology. F.S. Simmot lhe United Kingdom’s contributions to the development of aeronautics istry, combustion, and moto! Part 3. The development of the streamlined monoplane (the utics and aeronautics series, \ 1920s-1940s). J.A.D. Ackroyd, pp 217-268 E.L. Fleeman, p 115 DYNAMICS oplane Second Edition. D. Stinton, j5 459 Advanced combat aircraft performance assessment. A. Kutschera of air cushion craft. L. Yun and A. Bliaut and P.M. Render, pp 443-451 Fuzzy logic approach for estimation of longitudinal aircraft parameters. M.S. Yaacob, H. Jamaluddin and K.C. Wong, pp 585-594 COMPOSITES Linearised identification of the longitudinal flight dynamics of the on S DUCKI " ng performance of anti-symn solar powered airship Lotte. C.F. Eckersley and M.V. Cook, pp effect on behaviour of membr 571-581 . pp 595-605 Modelling of the hose and drogue in air-to-air refuelling. A.W. Bloy and M.M. Khan, pp 17-26. COMPUTATIONAL FLUID DYNAMICS The United Kingdom’s contributions to the development of aeronautics Maximising the impact of CFD in the design Part 3. The development of the streamlined monoplane (the \.J. Peace, pp 1920s-1940s). J.A.D. Ackroyd,p p 217-268 Mechanism of windward vortex shocks about Torsional/flexural response of large span wings to high altitude bodies. S.A. Prince and N. Qin,p p 507-519 turbulence. P.B.S. Lissaman and L.W. Brownlow, pp 325-335 Numerical modelling of mixing in jets from castel vles and R.Y.T. Wong, py ENVIRONMENTAL ENGINEERING transition boundary-lay Greene! by design the technology challenge. J.E. Green, Chairman equation. M.G. Higazy, pp of the Technology Sub-Group, pp 57-113 the vortex-fin interactior lhe impacts of aviation on the atmosphere. H.L. Rogers, D.S. Lee, Omar, K. Chongman and D.W. Raper, P.M. de F. Foster, C.W. Wilson and P.J. Newton, pp 521-546 and lift using velocity and vorticity field Zhu id J.M.R. Graham, pp 547-554 FLUID MECHANICS nology for global flow inst ind control Characterisation of wall flow topology in jet-in-crossflow interaction ley and S. Sherwin, pp 61‘ E.Y. Kwon and D. Chocinski, pp 393-398 esponses and system reduction Control of surface pressure fluctuations in reattaching flows by passive ] ler equations. A.L. Gaitonde means. R. Kumar and P.R. Viswanath, pp 669-674 Numerical modelling of mixing in jets from castellated nozzles. AJ and turbulent-flow computat Saddington, K. Knowles and R.Y.T. Wong, pp 643-652 d D. Drikakis, pp 349-384 Numerical prediction of transition boundary-layer flows using new c calculations using three intermittency transport equation. M.G. Higazy, pp 337-347 ructured dynamic grids. K.P Spectral/hp element technology for global flow instability and control V. Theofilis, D. Barkley and S. Sherwin, pp 619-625 nvestigation of high-spee K J Badcock and B.I GUIDANCE AND NAVIGATION Control techniques for autonomous launching of ship-based unmanned air vehicles (UAVs). M.R. Crump and C. Bil, pp 121 COMPUTATIONAL TECHNIQUES (GENERAL) 128 elastic computations using algebraic grid 3 HISTORY t of exit separation on aircraft The United Kingdom’s contributions to the development of aeronautics O-second certification trials Part 3. The development of the streamlined monoplane (the ues. S.J 3lake, E.R. Gale 1920s-1940s). J.A.D. Ackroppy 21d7-,26 8 illippidis, pp 1-16 ch for estimation of longitudina HYPERSONIC FLOW Jamaluddin and K.C. Wong \erodynamics of delta wings with flaps at hypersonic speeds. R ent methodology and mode Ramesh, pp 293-312 L. Walls and J. Jones. pp Pec hnical n The effecto f sequence of cavities on boundary mpressive buckling performance of anti layer separation at M = 8-2. Z. He, J. Xiong, ¢ Lebas and J.l 1e effect on behaviour of membrar ral couplit Stollery, pp 51-55 ougnian, pp 595-605 Utilising CFD in the investigation of high-speed unsteady spiked body flows. D. Feszty, K.J. Badcock and B.E. Richards, DEFENCE pp 161-174 Integrated review of stealth technology and its ro Rao and S. P. Mahulikar, pp 629-641 ICING The NREL micro tactical expendable (MITE) ait \ study of aerodynamic performance degradation on aerofoils and C. Bovais, R. Foch, H. McFarlane, C. Sullir Dahlburg, aircraft wings due to accreted ice. M. Khalid, F. Zhang and S Gardner and R. Ramamurti, pp 431-441 Chen, pp 461-472 LIFTING SURFACES Air travel — greener by design. J.L.Stollery, p 57 \ study of aerodynamic performance degradation on aerofoils and Greener by design — the technology challenge. J.E. Green, Chairman aircraft wings due to accreted ice. M. Khalid, F. Zhang and S. of the Technology Sub-Group, pp 57-113 Chen, pp 461-472 INDEX TO VOLUME 106 Aerodynamics of delta wings with flaps at hypersonic speeds. R. RELIABILITY Ramesh, pp 293-312. Reliability enhancement methodology and modelling the REMM Aeroelastic computations using algebraic grid motion. C.B. Allen, project. J. Marshall, L.W alls and J. Jones, pp 195-201 pp 559-570. Aeroelasticity of two-dimensional lifting surfaces via indicial function REMOTELY PILOTED VEHICLES (RPVs) approach. P. Marzocca, L. Librescu and G. Chiocchia, pp 147- Control techniques for autonomous launching of ship-based 153. unmanned air vehicles (UAVs). M.R. Crump and C. Bil, pp 121-128. Causes for discrepancies in ground effect analyses. TJ. Barber, E. Leonardi and D. Archer, pp 653-667. SAFETY Experimental investigation of trailing-edge devices at transonic A study of aerodynamic performance degradation on aerofoils and speeds. K. Richter and H. Rosemann, pp 185-193. aircraft wings due to accreted ice. M. Khalid, F. Zhang and S$ Measurements of leading-edge vortices on a 75° delta planform wing Chen, pp 461-472. at M = 2:5. 1.M. Milanovic and I.M. Kalkhoran, pp 39-49. Examining the effect of exit separation on aircraft evacuation perfor- Optimising wing lift distribution to minimise wake vortex hazard. mance during 90-second certification trials using evacuation W.R. Graham, pp 413-426. modelling techniques. SJ. Blake, E.R. Galea, S. Gwynne, PJ Prediction of drag and lift using velocity and vorticity fields. G. Zhu, Lawrence and L. Fillippidis, pp 1-16 P.W. Bearman and J.M.R. Graham, pp 547-554. Future air traffic management passing the key tests. P. Brooker, The use of pulse responses and system reduction for 2D unsteady pp 211-215. flows using the Euler equations. A.L. Gaitonde and D.P. Jones, pp Human factors in multi-crew flight operations. H.W. Orlady and 483-492. L.M. Orlady, pp 321-324. Torsional/flexural response of large span wings to high altitude The case for flight simulation in general aviation. DJ. Allerton, pp turbulence. P.B.S. Lissaman and L.W. Brownlow, pp 3 25-335. 607-612. Turbulence modelling and turbulent-flow computation in aeronautics. The perceived gap between need(ed) and mandated training “mind M.A. Leschziner and D. Drikakis, pp 349-384. the gap”. P.G. Richards, pp 427-430 Unsteady aerodynamic calculations using three-dimensional Euler equations on unstructured dynamic grids. K.P. Sinhamahapatra, SHOCK WAVES pp 269-276. Mechanism of windward vortex shocks about supersonic slender Wing aerodynamics and the science of compromise. Errata. J. Jupp, bodies. S.A. Prince and N. Qin, pp 507-519. p>. Normal shock wave-turbulent boundary-layer interactions in the presence of streamwise slots and grooves. A.N. Smith, H. Babinsky, MAN-POWERED FLIGHT J.L. Fulker and P.R. Ashill, pp 493-500. The human-powered helicopter. A. Filippone, pp 613-618. Aircrew mission training via distributed simulation the potential MATERIALS in NATO. B. Tomlinson, pp 155-159. Micro-foamed structural materials for micro-aircraft. E. O°’K eefe, M. Examining the effect of exit separation on aircraft evacuation perfor Swan, R. Jones, V.G ergly and N. Cameron, pp 385-392. mance during 90-second certification trials using evacuation mod- elling techniques. SJ. Blake, E.R. Galea, S. Gwynne, PJ. METEOROLOGY Lawrence and L. Fillippidis, pp 1-16 Greener by design — the technology challenge. J.E. Green, Chairman Modelling of the hose and drogue in air-to-air refuelling. A.W. Bloy of the Technology Sub-Group, pp 57-113 and M.M. Khan, pp 17-26. The impacts of aviation on the atmosphere. H.L. Rogers, D.S. Lee, Simulation and collective training creating a total experience. E D.W. Raper, P.M. de F. Foster, C.W. Wilson and PJ. Newton, pp Smith and H.M. Mcintyre, pp 129-136 521-546. The case for flight simulation in general aviation. DJ. Allerton, pp 607-612 PROPULSION Active control of fan noise from high-bypass ratio aeroengines: STRENGTH ANALYSIS experimental results. L. Enghardt, U. Tapken, W. Neise. P The compressive buckling performance of anti-symmetric composite Schimming, R. Maier and J. Zillmann, pp 501-506. laminates and the effect on behaviour of membrane-flexural Aerodynamic performances of propellers with parametric considerations coupling. J. Loughlan, pp 595-605 on the optimal design. S. D’Angelo, F. Berardi and E. Minisci, pp The United Kingdom’s contributions to the development of aeronautics 313-320. Part 3. The development of the streamlined monoplane (the Greener by design — the technology challenge. J.E. Green, Chairman 1920s-1940s). J.A.D. Ackroyd,p p 217-268 of the Technology Sub-Group, pp 57-113 Integrated engine management: a new approach to health monitoring TESTING FACILITIES AND TECHNIQUES and control of gas turbine aero-engines. JJ. Gribble and G.J. Effect of tracer particle characteristics on visualisation of delta wing Dadd, pp 203-209. vortices. D.1. Greenwell, pp 473-482 Letter. R. FitzPatrick, p 215. Fuzzy logic approach for estimation of longitudinal aircraft parameters Maximising the impact of CFD in the design office: ARA’s role. M.S. Yaacob, H. Jamaluddin and K.C. Wong, pp 585-594 A.J. Peace, pp 675-685. Integrated engine management: a new approach to health monitoring Numerical modelling of mixing in jets from castellated nozzles. AJ. and control of gas turbine aero-engines. J.J. Gribble and GJ Saddington, K. Knowles and R.Y.T. Wong, pp 643-652. Dadd, pp 203-209 The impacts of aviation on the atmosphere. H.L. Rogers, D.S. Lee, Surface thermometry by laser-induced fluorescence of Dy**:YAG D.W. Raper, P.M. deF. Foster, C.W. Wilson and P.J. Newton, pp K. Kontis, Y. Syogenji and N. Yoshikawa, pp 453-457 521-548. The United Kingdom's contributions to the development of aeronautics. TRAINING Part 3. The development of the streamlined monoplane (the Aircrew mission training via distributed simulation the potential 1920s-1940s). J.A.D. Ackroyd, pp 217-268. in NATO, B. Tomlinson, pp 155-159 690 THE AERONAUTICAL JOURNAI DECEMBER 2002 Simulation and collective training creating a total experience. | Unsteady aerodynamic calculations using three-dimensional Euler Smith and H.M. McIntyre, pp 129-136. equations on unstructured dynamic grids. K.P. Sinhamahapatra The case for flight simulation in general aviation. DJ. Allerton, pp pp 269-276 Utilising CFD in the investigation of high-speed unsteady spiked between need(ed) and mandated training “mind body flows. D. Feszty, K.J. Badcock and B.E. Richards, pp 161-174 ichards, pp 427-430 V/STOL \utorotating rotor with ornithopter-like flapping blades. V. Savoy TRIBUTE and M. Raikov, pp 399-409 Dawn Steele, p 336 Flow visualisation of the orthogonal blade-vortex interaction using particle image velocimetry. J.M. Early, R.B. Green and F.N UNSTEADY AERODYNAMICS omg CoOnNtTrO!o l ¢ of surface iporieasmsauier e esc fluctuations in reatta‘cih ing flows by7 % passive lhe h; uman-powered helicopter. A. Filippone, pp 613S-6a1 8 sans. R. Kumar and P.R. Viswanath, pp 669-67 liltrotor development to meet public acceptability targe Spectral/hp element technology for global flow instability and control \ V. Theofilis, D. Bark4l5 ey and S.a ieS herwin, pp 619-625- Reber, pp 33-38 rhe use of pul esponses and system reduction for 2D unsteady WAKES flows using the Euler equations. A.L. Gaitonde and D1 ». Jones, pp Technical note. Near field study of vortex attenuation using wing-tip 183-497 blowing. R.G. Simpson, N.A. Ahmed and R.D. Archer, pp 117-120 lurbulence modelling and turbulent-flow computation in aeronautics Optimising wing lift distribution to minimise wake vortex M.A. Leschziner and D. Drikakis, pp 349-384 W.R. Graham, pp 413-426 Author Index ACKROYD, J.A.D. BEARMAN, P.W., ZHU, G. and GRAHAM, J.M.R. lhe United Kingdom's contributions to the development of aeronautic Prediction of drag and lift using velocity and vorticity field Part 3. The development of the streamlin yplane (th 554 ) 1-268 BERARDI,F ., D ANGELO, S. and MINISCI, E. AHME D, N.A., SIMPSON, R.G. and ARCHER, R.D. \erodynamic performanceso f propellersw i Near field study of vortex attenuat ° Wing-tip on the optin 313-3 BIL, C. and CRUMP, MLR. ALLEN, C.B. Control technique r autonomous Aeroelastic computati using algebri rid mot pp 559-570 unmanned air vel S AVs). pp 12 ALLERTON, D.J. BLAKE, S.J., GALEA, E.R., GWYNNS.E, ,LA WRENCE, The case for flight s lation in general aviatio | and FILLIPIDIS, L. ct of exit separation on all ARCHER, D., BARBER, T.J. and LEONARDI , ance during 90-second certification Causes for discrepancies in ground effect analys ( 667 modelling techniques,p p | ARCHER, R.D., SIMPSON, R.G. and AHMED, N.A. BLOY, A.W. and KHAN, M.M. Technical note. Near field study of vortex attent I ng-tip Modelling of the hose and dri BOVAIS, C., KELLOGG,J ., FOCR.H, M,cFA RLANE, ASHILL, P.R., SMITH, . BABINSKY, H. and FULKER, _ SULLIVAN, C., DAHLBURG, J., GARDNER, J. and Normal shock vave-ti storied boundar y-layer sint RAMAMURTI,.R presence of streamwise slots and grooves, pp 493 The NRL micro tactical expendable (MITE BABINSH.K, SYMI,TH , A.N., FULKER, J.L. and ASHILL, P.R. BROOKER, P. Normal shock wave-turbulent boundary-layer interactions in th Future air traf presenceo f streamwise slots and grooves, pp 49 BROWNLOW, L.W. and LISSAMAN, P.B.S. BADCOCK, K.J., FESZTY, D. and RICHARDSB,.E . ee ee ae ee eee ee ee Utilising CFD in the investigation of high-sp re body flows.p p 161-174 cial CAMERON, N., O’KEEFE, E., SWAN, M., JONESR., an d ‘ ; ' GERGLY,V . BAGSHAW, M. and LOWER, M.C. ; Micro-foamed structural materialsfo r micro-aircraft,p p 385 Hearing loss on the flight deck origin and 1 CHEN,S., KHALID, M. and ZHANG, F. BARBER, T.J., LEONARDI, E. and ARCHER, D \ study of aerodynamic performance degradation on aerofoils and Causes for discrepancies in ground effect analyses aircraft wings due to accreted ice, pp 461-472 BARKLEY, D., THEOFILIS, V. and SHERWIN, S. CHIOCCHIA, G., MARZOCCA, P. and LIBRESCU, L. Spectral/hp element technology for global flow instability and control, Aeroelasticity of two-dimensional lifting surfaces via indicial function pp 619-625. approach, pp 147-153 INDEX TO VOLUME 106 CHOCINSKI, D. and KWON, E.Y. FITZPATRICK, R. Characterisation of wall flow topology in jet-in-crossflow interaction, Letter, p 215 pp 393-398. FOCH, R., KELLOGG, J., BOVAIS, C., McFARLANE, H., CHONGMAN, K., OMAR, A.A. and OH-HYUN, R. SULLIVAN, C., DAHLBURG, J., GARDNER, J. and Numerical simulation of the vortex-fin interaction over a tangent- RAMAMURTI,R. ogive cylinder, pp 175-184. The NRL micro tactical expendable (MITE) air vehicle, pp 431-441 COOK, M.V. and ECKERSLEY, C.F. FOSTER, P.M. de F., ROGERS, H.L., LEE, D.S., RAPER, D.W., Linearised identification of the longitudinal flight dynamics of the WILSON, C.W. and NEWTON, P.J. solar powered airship Lotte, pp 571-581 The impacts of aviation on the atmosphere, pp 521-546 COOPER, J.E., SEDAGHAT, A., WRIGHT, J.R. and LEUNG, FULKJ.EL.,R SM,ITH , A.N., BABINSKHY. ,an d ASHILL, P.R. AY... Normal shock wave-turbulent boundary-layer interactions in the Limit-cycle oscillation prediction for non-linear aeroelastic systems, presence of streamwise slots and grooves, pp 493-500 pp 27-32. GAITONDE, A.L. and JONES, D.P. COTON, F.N., EARLY, J.M. and GREEN, R.B. The use of pulse responses and system reduction for 2D unsteady Flow visualisation of the orthogonal blade-vortex interaction using flows using the Euler equations, pp 483-492 particle image velocimetry, pp 13 145 GALEA, E.R., BLAKE, S.J., GWYNNE, S., LAWRENCE, PJ. CRUMP, M.R. and BIL, C. and FILLIPIDIS, L. Control techniques for autonomous launching of ship-based Examining the effect of exit separation on aircraft evacuation perfor unmanned air vehicles (UAVs), pp 121-128 mance during 90-second certification trials using evacuation mod elling techniques, pp 1-16 DADD, G.J. and GRIBBLE, J.J. Integrated engine management: a new approach to health monitoring GARDNER,J .,K ELLOGG, J., BOVAIS, C., FOCH, R., and control of gas turbine aero-engines, pp 203-209 McFARLANE, H., SULLIVAN, C., DAHLBURG,J . and RAMAMURTI, R. DAHLBURG,J ., KELLOGG,J ., BOVAIS, C., FOCH, R., The NRL micro tactical expendable (MITE) air vehicle, pp 431-441 McFARLANE, H., SULLIVAN, C., GARDNER, J. and RAMAMURTI,R. GERGLY, V., O°KEEFE, E., SWAN, M., JONES, R. and lhe NRL micro tactical expendable (MITE) air vehicle, pp 431-441. CAMERON,N. Micro-foamed structural materials for micro-aircraft, pp 385-392 D’ ANGELO, S., BERARDI, F. and MINISCI, E. \erodynamic performances of propellers with parametric considerations GRAHAM, J.M.R., ZHU, G. and BEARMAN, P.W, on the optimal design, pp 313-320 Prediction of drag and lift using velocity and vorticity fields, pp 547 554 DRIKAKIS, D. and LESCHZINER, M.A. lurbulence modelling and turbulent-flow computation in aeronau GRAHAM, W.R. tics, pp 349-384 Optimising wing lift distribution to minimise wake vortex hazard, pp 413-426 EARLY, J.M., GREEN, R.B. and COTON, F.N. Flow visualisation of the orthogonal blade-vortex interaction using GREEN, J.E. (Chairman of the Technology Sub-Group) particle image velocimetry, pp 137-145 Greener by design — the technology challenge, pp 57-113 ECKERSLEY, C.F. and COOK, M.YV. GREEN, R.B., EARLY, J.M. and COTON, F.N. Linearised identification of the longitudinal flight dynamics of the Flow visualisation of the orthogonal blade-vortex interaction using solar powered airship Lotte, pp 571-581 particle image velocimetry, pp 137-145 ENGHARDT, L., TAPKEN, U., NEISE, W., SCHIMMING, P., GREENWELL, D.1. MAIER, R. and ZILLMANN, J. Effect of tracer particle characteristics on visualisation of delta wing Active control of fan noise from high-bypass ratio aeroengines: ex vortices, pp 473-482 perimental results, pp 501-506 GRIBBLE, J.J. and DADD, G.J. FESZTY, D., BADCOCK, K.J. and RICHARDS, B.E. Integrated engine management: a new approach to health monitoring Utilising CFD in the investigation of high-speed unsteady spiked and control of gas turbine aero-engines, pp 203-209 body flows, pp 161-174. GWYNNE, S., BLAKE, S.J., GALEA, E.R., LAWRENCE, P.J. FILIPPONE,A . and FILLIPIDIS, L. lhe human-powered helicopter, pp 613-618 Examining the effect of exit separation on aircraft evacuation pertfor- mance during 90-second certification trials using evacuation mod- FILLIPIDIS, L., BLAKE, S.J., GALEA, E.R., GWYNNE, S. and elling techniques, pp 1-16 LAWRENCE, P.J. Examining the effect of exit separation on aircraft evacuation perfor- HE, Z., XIONG, J., LEBAS, C. and STOLLERY, J.L. mance during 90-second certification trials using evacuation Technical note. The effect of a sequence of cavities on boundary- modelling techniques, pp 1-16 layer separation at M = 8-2, pp 51-55. [THE AERONAUTICAL JOURNAI DECEMBER 2002 HIGAZY, M.G. LEBAS, C., HE, Z., XIONG,J .a nd STOLLERY, J.L. | pred f transition boundary-layer f Technical note. The effect of a sequence of cavities on boundary- pt ort equation, pp 337-347 layer separation at M = 8-2, pp 51-55 JAMALUDDIN, H., YAACOB, M.S. and WONG, K.C. LEE, D.S., ROGERS, H.L., RAPER, D.W., FOSTER, P.M. de ic approach for estimation of longitudinal air F., WILSON, C.W. and NEWTON, P.J. The impacts of aviation on the atmosphere, pp 521-546 .and GAITONDE, A LEONARDI, E., BARBER, T.J. and ARCHER, D. responses and system reductio1 Causes for discrepancies in ground effect analyses, pp 653-667 r equations, pp 483-492 LESCHZINER, M.A. and DRIKAKIS, D. .J.. MARSHALL, J. and WALLS, L. Turbulence modelling and turbulent-flow computation in aeronautics, ity enhancement methodology and modelli the REMM pp 349-384 n LEUNG, A.Y.T., SEDAGHAT, A., COOPER, J.E. and JONES, R., O°KEEFE, E., SWAN, M., GERGLY, V. and WRIGHT, J.R CAMERON,N . Limit-cycle oscillation prediction for non-linear aeroelastic systems Micro-toamed structur naterialsfo r micro-aircraft JUPP, J. LIBRESCU, L., MARZOCCA, P. and CHIOCCHIA, G. Wing aerodyna cS and the science of comprom Aeroelasticity of two-dimensional lifting surfaces via indicial function approach, pp 147-153 KALKHORAN, I.M. and MILANOVIC, I.M. Measurements « eading-edge vorticeosn a 75 LISSAMAN, P.B.S. and BROWNLOW, L.W. tM =2°5,1 orsional/flexural response of large span wings to high altitude turbulence KAMEL, O.M. and SOLIMAN, ASS. Velocity correction generalised Hohmann an LOUGHLAN, J. SS55_S58 Che compressive buckling performance of anti-symmetric composite linates and the effect behaviour of membrane-flexural KELLOGJG.,, B OVAIS, C., FOCHR.,, McFARLANE, H., coupling. pp 595-605 SULLIVAN, C., DAHLBURG, J., GARDNER, J. and RAMAMURTI,R. LOWER, M.C. and BAGSHAW, M. e NRL micro tactic il expendable (MITE ) all Hearing loss on the flight deck origin and remedy, pp 2 KHALID, M., ZHANG, F. and CHEN,S . McFARLANE, H., KELLOGG, J., BOVAIS, C., FOCH, R., \ study of ae nic performance degradat SULLIVAN, C., DAHLBURG, J., GARDNEJR. ,an d creted Ice pp 4“611 474% RAMAMURTI,R. he NRL micro tactical expendable (MITE) air vehicle, pp 431-441 KHAN, M.M. and BLOY, A.W. Modelling of the hose and drogue in air-to-au Mc:NHT.M.Y anRd SEMIT,H, E. Simulation and collective training | experience, pp KNOWLES, K., SADDINGTON, A.J. and WONG, R.Y. 129-136 Numerical modelli »f mixing in jets from cast ! (6 4 MAHULIKAR,S. P. and RAO, G.A. Integrated review of stealth technology and its role in airpowet KONTIS,K ., SYOGENJI, Y. and YOSHIKAWA, N. 629-64] by laser-induced fluores MAIER, R., ENGHARDT, L., TAPKEN, U., NEISE, W SCHIMP.M anId ZNILLGMAN,N, J. KUMAR, R. and VISWANATH, P.R. Active control of fan noise from high-bypass ratio aeroengines Control of surface pressure fluctuations in experimental results, pp 501-506 passive means, pp 669-674 MANS, K. and MARSHALL, D KI TOLEERA A, A. and RENDER, P.M. rhe origins of greener by design, p 57 Advanced combat aircraft performance assessme MARSHALL, D. and MANS, K. KWON, E.Y. and CHOCINSKI, D. rhe origins of greener by design, p 5 Characterisation of wall flow topology in jet-in-crossflow interaction pp 393-398 MARSHALL, J., WALLS, L. and JONES,J . Reliability enhancement methodology and modelling the REMM LAWRENCE, P.J., BLAKE, S.J., GALEA, E.R., GWYNNE, S project, pp 195-201 and FILLIPIDIS, L. Examining the effect of exit separation on aircraft evacuation perfor MARZOCCA, P., LIBRESCU, L. and CHIOCCHIA,G. mance during 90-second certification trials using evacuation Acroelasticity of two-dimensional lifting surfaces via indicial function modelling techniques, pp 1-16. approach, pp 147-153 INDEX TO VOLUME 106 MILANOVIC, I.M. and KALKHORAN, LM. RENDEP.RM., a nd KUTSCHERA, A. Measurements of leading-edge vortices on a 75° delta planform wing Advanced combat aircraft performance assessment, pp 443-451 at M = 2:5, pp 39-49. RICHARDS, B.E., FESZTY, D. and BADCOCK, K.J. MINISCI, E., DDANGELO, S. and BERARDI, F. Utilising CFD in the investigation of high-speed unsteady spiked Aerodynamic performances of propellers with parametric considerations body flows, pp 161-174 on the optimal design, pp 313-320 RICHARDS, P.G. NEISE, W., ENGHARDT, L., TAPKEN, U., SCHIMMING, P., The perceived gap between need(ed) and mandated training “mind MAIER, R. and ZILLMANN, J. the gap”, pp 427-430 Active control of fan noise from high-bypass ratio aeroengines experimental results, pp 501-506 RICHTER, K. and ROSEMANN, H. Experimental investigation of trailing-edge devices at transonic NEWTON, P.J., ROGERS, H.L., LEE, D.S., RAPER, D.W., speeds, pp 185-193 FOSTER, P.M. de F. and WILSON, C.W. Che impacts of aviation on the atmosphere, pp 521-546 ROGERS, H.L., LEE, D.S., RAPER, D.W., FOSTER, P.M. de OH-HYUN, R., OMAR, A.A. and CHONGMAN, K. F., WILSON, C.W. and NEWTON, P.J. Numerical simulation of the vortex-fin interaction over a tangent- The impacts of aviation on the atmosphere, pp 521-546 ogive cylinder, pp 175-184 ROSEMANN, H. and RICHTER, K. O°’ KEEFE, E., SWAN, M., JONES, R., GERGLY, V. and Experimental investigation of trailing-edge devices at transonic CAMERON,N. speeds, pp 185-193 Micro-foamed structural materials for micro-aircraft, pp 385-392 SADDINGTON, A.J., KNOWLES, K. and WONG, R.Y.T. OMAR, A.A., CHONGMAN, K. and OH-HYUN, R. Numerical modelling of mixing in jets from castellated nozzles, pp Numerical simulation of the vortex-fin interaction over a tangent 643-65? ogive cylinder, pp 175-184 SAVOV, V. and RAIKOV, M. ORLADY, H.W. and ORLADY, L.M. Autorotating rotor with ornithopter-like flapping blades, pp 399-409 Human factors in multi-crew flight operations, pp 321-324 SCHIMMING,P ., ENGHARDT, L., TAPKEN, U., NEISE, W., ORLADY, L.M. and ORLADY, H.W. MAIERR., a nd ZILLMANN, J. Human factors in multi-crew flight operations, pp 321-324 Active control of fan noise from high-bypass ratio aeroengines experimental results, pp 501-506 PEACE, A.J. Maximising the impact of CFD in the design office: ARA’s role., pp SEDAGHAT, A., COOPER, J.E., WRIGHT, J.R. and LEUNG, 675-685. Awe Limit-cycle oscillation prediction for non-linear aeroelastic systems, PRINCS.EA. ,a nd QIN, N. pp 27-32 Mechanism of windward vortex shocks about supersonic slendet bodies, pp 507-519 SHERWIN, S., THEOFILIS, V. and BARKLEY, D. Spectral/hp element technology for global flow instability and control QIN, N. and PRINCE, S.A. pp 619-625 Mechanism of windward vortex shocks about supersonic slender bodies, pp 507-519 SIMPSON, R.G., AHMED, N.A. and ARCHER, R.D. Technical note. Near field study of vortex attenuation using wing-tip RAIKOV, M. and SAVOV, V. blowing, pp 117-120 Autorotating rotor with ornithopter-like flapping blades, pp 399-409 SINHAMAHAPATRA, K.P. RAMAMURTI, R., KELLOGG, J., BOVAIS, C., FOCH, R., Unsteady aerodynamic calculations using three-dimensional Euler McFARLANE, H., SULLIVAN, C., DAHLBURG, J. and equations on unstructured dynamic grids, pp 269-276 GARDNER,J . The NRL micro tactical expendable (MITE) air vehicle, pp 431-441 SMITH, A.N., BABINSKY, H., FULKER, J.L. and ASHILL, PR. RAMESH,R . Normal shock wave-—turbulent boundary-layer interactions in the Aerodynamics of delta wings with flaps at hypersonic speeds, pp presence of streamwise slots and grooves, pp 493-500 293-312. RAO, G.A. and MAHULIKAR, S.P. SMITH, E. and McINTYRE, H.M. Integrated review of stealth technology and its role in airpower, pp Simulation and collective training creating a total experience, pp 629-641 129-136 RAPER, D.W., ROGERS, H.L., LEE, D.S., FOSTER, P.M. de SOLIMAN, A\S. and KAMEL, O.M. F., WILSON, C.W. and NEWTON, P.J. Velocity corrections in generalised Hohmann and bi-elliptic transfer The impacts of aviation on the atmosphere, pp 521-546 REBER, R.R. STOLLERY, J.L. Tiltrotor development to meet public acceptability targets, pp 33-38. Air travel — greener by design, p 57 694 THE AERONAUTICAL JOURNAI DECEMBER 2002 STOLLERY, J.L., HE, Z., XIONG,J . and LEBAS, C. WILSON, C.W., ROGERS, H.L., LEE, D.S., RAPER, D.W., fechnical note. The effect of a sequence of cavities on boundary- FOSTER, P.M. de F. and NEWTON, PJ. layer separation at M = 8-2, pp 51-55. The impacts of aviation on the atmosphere, pp 521-546 WONG, K.C., YAACOB, M.S. and JAMALUDDIN, H. SULLIVAN, C., KELLOGG, J., BOVAIS, C., FOCH, R., Fuzzy logic approach for estimation of longitudinal aircraft parameters, McFARLANE, H., DAHLBURG,J ., GARDNER, J. and pp 585-594 RAMAMURTI,R. The NRL micro tactical expendable (MITE) air vehicle, pp 431-441 WONG, R.Y.T., SADDINGTON, A.J. and KNOWLES, K. Numerical modelling of mixing in jets from castellated nozzles, pp SWAN, M., O’KEEFE, E., JONES, R., GERGLY, V. and 643-652 CAMERON,N. Micro-foamed structural materials for micro-aircraft, pp 385-392 WRIGHT, J.R., SEDAGHAT, A., COOPER, J.E. and LEUNG, A.¥.i. SYOGENJI, Y., KONTIS, K. and YOSHIKAWA, N. Limit-cycle oscillation prediction for non-linear aeroelastic systems, Surface thermometry by laser-induced fluorescence of Dy*+:YAG, pp 27-32 pp 453-457 XIONG, J., HE, Z., LEBAS, C. and STOLLERY, J.L. Technical note. The effect of a sequence of cavities on boundary- TAPKEN, U., ENGHARDT, L., NEISE, W., SCHIMMING, P., layer separation at M = 8-2, pp 51-55. MAIER, R. and ZILLMANN,J . Active control of fan noise from high-bypass ratio aeroengines YAACOB, MSS., JAMALUDDIN, H. and WONG, K.C. experimental results, pp 501-506. Fuzzy logic approach for estimation of longitudinal aircraft parameters, pp 585-594 THEOFILIS, V., BARKLEY, D. and SHERWIN, S. Spectral/hp element technology for global flow instability and control, YOSHIKAWA, N., KONTIS, K. and SYOGENJI, Y. pp 619-625 Surface thermometry by laser-induced fluorescence of Dy*+:YAG, pp 453-457 TOMLINSON, B. ZHANG, F., KHALID, M. and CHEN, S. Aircrew mission training via distributed simulation the potential \ study of aerodynamic performance degradation on aerofoils and in NATO, pp 155-159 aircraft wings due to accreted ice, pp 461-472 VISWANATH, P.R. and KUMAR, R. ZHU, G., BEARMAN, P.W. and GRAHAM, J.M.R. Control of surface pressure fluctuations in reattaching Prediction of drag and lift using velocity and vorticity fields, pp 547-554 passive means, pp 669-674 ZILLMANN, J., ENGHARDT, L., TAPKEN, U., NEISE, W., WALLS, L., MARSHALL,J . and JONES,J . SCHIMMING, P. and MAIER, R. Reliability enhancement methodology and modelling the REMM Active control of fan noise from high-bypass ratio aeroengines project, pp 195-201 experimental results, pp 501-506 Volume CVI Number 1055 January pp 1-55 Number 1056 February pp 57-115 Number 1057 March pp 117-159 Number 1058 April pp 161-215 Number 1059 May pp 217-291 Number 1060 June pp 293-347 Number 1061 July pp 349-411 Number 1062 \ugust pp 413-459 Number 1063 September pp 461-519 Number 1064 October pp 521-583 Number 1065 November pp 585-627 Number 1066 December pp 629-695

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