The Aeronautical Journal 2001: Vol 105 Index

9 Pages·2001·2.5 MB·English

THE AERONAUTICAL JOURNAL DECEMBER 2001
THE AERONAUTICAL JOURNAL
OF THE ROYAL AERONAUTICAL SOCIETY
Volume CV
January-December 2001
Subject Index
AERODYNAMICS Helicopter encounters with aircraft vortex wakes. G.D. Padfield and
A data exchange method for fluid-structure interaction problems G.P. Turner. pp 1-8
G.S.L. Goura, K.J. Badcock, M.A. Woodgate and B.E. Richards. Implicit method for the time marching analysis of flutter. G.S.L.
pp 215-221. Goura, K.J. Badcock, M.A. Woodgate and B.E. Richards, pp 199-
Aeroservoelastic simulation by time-marching. L. Djayapertapa and 214
C.B. Allen, pp 667-678 Multigrid acceleration of an upwind Euler method for hovering rotor
An assessment of the 2D vortex method in aircraft wake simulation flows. C.B. Allen, pp 517-524.
W.R. Graham, pp 653-666 Multigrid upwind Euler/Navier-Stokes computation on adaptive
An eddy-viscosity limited algebraic stress model for shock—boundary unstructured meshes. Y. Zheng and L. He, pp 173-184.
layer interaction. N. Qin and G. Richardson, pp 105-118 Non-inertial multiblock Navier-Stokes calculation for hovering rotor
A neural network approach to the calibration of a flush air data system flowfields using relative velocity approach. B. Zhong and N. Qin,
W.J. Crowther and P.J. Lamont. pp 85-95. pp 379-389
An experimental and numerical study of synthetic jet flow. G. Hong, Numerical and experimental investigations of air-jet vortex generators
S.G. Mallinson and J.A. Reizes, pp 41-49 in streamwise pressure gradients. N.P. Lewington, F.S. Henry.
A new moving-boundary algorithm with application to SRM internal D.J. Peake and C. Singh, pp 401-407
ballistics. S.M.H. Karimian and A. Amoli. pp 697-705 Performance enhancement evaluation of an actuated trailing edge
A numerical study of the application of vane and air-jet vortex flap. W. Chan and A. Brocklehurst, pp 391-399.
generators. C. Kiipper and F.S. Henry, pp 255-265. Potential fuel savings due to hybrid laminar flow control under oper-
Assessment of turbulence model performance for transonic flow ove ational conditions. T.M. Young and J.P. Fielding, pp 581-588.
an axisymmetric bump. R.G.M. Hasan and J.J. McGuirk. pp 17-31 QUACC, a novel method for predicting unsteady flows — including
A strategic European approach to aerodynamics research, technology propellers and store release. D.L. Hunt, M. Childs and M. Maina,
and development. P.C. Dexter, pp 451-457 pp 427-434.
Development and application of farfield drag extraction techniques Reynolds-stress modelling of afterbody flows. M.A. Leschziner, P.
for complex viscous flows. D.L. Hunt, pp 161-169. Batten and T.J. Craft, pp 297-306
Experimental and numerical investigation of wind tunnel wall inter Simulation of flows within an electrostatic ion shruster for space
ference near Mach one. M. Mokry, M. Khalid, Y. Mébarki and A missions. M. Jugroot and J.K. Harvey, pp 613-618.
Rebaine, pp 589-596. The effect of wing planform shape on dynamic stall. F.N. Coton,
Experimental investigation into transonic flows over tandem cavities R.A.McD. Galbraith and R.B. Green, pp 151-159.
D. Bray, K. Knowles and N. Taborda, pp 119-124. Transition and separation control in the leading edge region. P.W.C.
Experimental study on the flow and noise characteristics of under- Wong, M. Maina and A.M. Cobbin, pp 371-378.
expanded notched slot jets. S.B. Verma and E. Rathakrishnan, pp Trimmed deep stall on the F-16 Fighting Falcon. L.D. Evangelou.,
267-275. A.W. Self. J.E. Allen and S. Lo, pp 679-683.
Extensions to Maskell’s theory for blockage effects on bluff bodies Understanding subsonic and transonic cavity flows. K.J. Badcock,
in a closed wind tunnel. J.E. Hackett and K.R. Cooper, pp 409-418. B.E. Edwards and J. Henderson, pp 77-84.
Flow regimes associated with yawed rectangular cavities. M. Czech, Visualisation of flow separation with shear-sensitive liquid crystals.
T. Maurides, E. Savory and N. Toy, pp 125-134. S. O'Brien and S. Zhong, pp 597-602.
Future challenges for powerplant aerodynamic integration in combat Wing aerodynamics and the science of compromise. J. Jupp, pp 633-
aircraft. M.G. Philpot, pp 335-342. 641.
THE AERONAUTICAL JOURNAL DECEMBER 2001
THE AERONAUTICAL JOURNAL
OF THE ROYAL AERONAUTICAL SOCIETY
Volume CV
January-December 2001
Subject Index
AERODYNAMICS Helicopter encounters with aircraft vortex wakes. G.D. Padfield and
A data exchange method for fluid-structure interaction problems G.P. Turner. pp 1-8
G.S.L. Goura, K.J. Badcock, M.A. Woodgate and B.E. Richards. Implicit method for the time marching analysis of flutter. G.S.L.
pp 215-221. Goura, K.J. Badcock, M.A. Woodgate and B.E. Richards, pp 199-
Aeroservoelastic simulation by time-marching. L. Djayapertapa and 214
C.B. Allen, pp 667-678 Multigrid acceleration of an upwind Euler method for hovering rotor
An assessment of the 2D vortex method in aircraft wake simulation flows. C.B. Allen, pp 517-524.
W.R. Graham, pp 653-666 Multigrid upwind Euler/Navier-Stokes computation on adaptive
An eddy-viscosity limited algebraic stress model for shock—boundary unstructured meshes. Y. Zheng and L. He, pp 173-184.
layer interaction. N. Qin and G. Richardson, pp 105-118 Non-inertial multiblock Navier-Stokes calculation for hovering rotor
A neural network approach to the calibration of a flush air data system flowfields using relative velocity approach. B. Zhong and N. Qin,
W.J. Crowther and P.J. Lamont. pp 85-95. pp 379-389
An experimental and numerical study of synthetic jet flow. G. Hong, Numerical and experimental investigations of air-jet vortex generators
S.G. Mallinson and J.A. Reizes, pp 41-49 in streamwise pressure gradients. N.P. Lewington, F.S. Henry.
A new moving-boundary algorithm with application to SRM internal D.J. Peake and C. Singh, pp 401-407
ballistics. S.M.H. Karimian and A. Amoli. pp 697-705 Performance enhancement evaluation of an actuated trailing edge
A numerical study of the application of vane and air-jet vortex flap. W. Chan and A. Brocklehurst, pp 391-399.
generators. C. Kiipper and F.S. Henry, pp 255-265. Potential fuel savings due to hybrid laminar flow control under oper-
Assessment of turbulence model performance for transonic flow ove ational conditions. T.M. Young and J.P. Fielding, pp 581-588.
an axisymmetric bump. R.G.M. Hasan and J.J. McGuirk. pp 17-31 QUACC, a novel method for predicting unsteady flows — including
A strategic European approach to aerodynamics research, technology propellers and store release. D.L. Hunt, M. Childs and M. Maina,
and development. P.C. Dexter, pp 451-457 pp 427-434.
Development and application of farfield drag extraction techniques Reynolds-stress modelling of afterbody flows. M.A. Leschziner, P.
for complex viscous flows. D.L. Hunt, pp 161-169. Batten and T.J. Craft, pp 297-306
Experimental and numerical investigation of wind tunnel wall inter Simulation of flows within an electrostatic ion shruster for space
ference near Mach one. M. Mokry, M. Khalid, Y. Mébarki and A missions. M. Jugroot and J.K. Harvey, pp 613-618.
Rebaine, pp 589-596. The effect of wing planform shape on dynamic stall. F.N. Coton,
Experimental investigation into transonic flows over tandem cavities R.A.McD. Galbraith and R.B. Green, pp 151-159.
D. Bray, K. Knowles and N. Taborda, pp 119-124. Transition and separation control in the leading edge region. P.W.C.
Experimental study on the flow and noise characteristics of under- Wong, M. Maina and A.M. Cobbin, pp 371-378.
expanded notched slot jets. S.B. Verma and E. Rathakrishnan, pp Trimmed deep stall on the F-16 Fighting Falcon. L.D. Evangelou.,
267-275. A.W. Self. J.E. Allen and S. Lo, pp 679-683.
Extensions to Maskell’s theory for blockage effects on bluff bodies Understanding subsonic and transonic cavity flows. K.J. Badcock,
in a closed wind tunnel. J.E. Hackett and K.R. Cooper, pp 409-418. B.E. Edwards and J. Henderson, pp 77-84.
Flow regimes associated with yawed rectangular cavities. M. Czech, Visualisation of flow separation with shear-sensitive liquid crystals.
T. Maurides, E. Savory and N. Toy, pp 125-134. S. O'Brien and S. Zhong, pp 597-602.
Future challenges for powerplant aerodynamic integration in combat Wing aerodynamics and the science of compromise. J. Jupp, pp 633-
aircraft. M.G. Philpot, pp 335-342. 641.
INDEX TO VOLUME 105 707
AEROELASTICITY Zarchan, P. and Musoff, H. Fundamentals of Kalman Filtering: A
A fully distributed unstructured Navier-Stokes solver for large-scale Practical Approach. Progress in Astronautics and Aeronautics
aeroelasticity computations. G. Barakos, M. Vahdati, A.I. Sayma, Series, Vol 190, p 400.
C. Bréard and M. Imregun, pp 419-426. Zipfel, P.H. Modelling and Simulation of Aerospace Vehicle Dynamics.
Implicit method for the time marching analysis of flutter. G.S.L. p 294.
Goura, K.J. Badcock, M.A. Woodgate and B.E. Richards, pp 199-
214. BOOK REVIEWS — BY TITLE
Laplace-domain approximation to the transfer functions of a rotor Air and Spaceborne Radar Systems: An Introduction. P. Lacomme et
blade in forward flight. F. Nitzsche, pp 233-240. al, p 684.
Aircraft Conceptual Design Synthesis. D. Howe, p 160.
BOOK REVIEWS — BY AUTHOR Aircraft Structures for Engineering Students — third edition. T.H.G.
Adamy, D. EW101: A First Course in Electronic Warfare, p 684. Megson, p 607.
Bramwell, A.R.S.. Done, G. and Balmford, D. Bramwell’s Heli- Airframe Structural Design: Practical Design Information and Data.
copter Dynamics — second edition, p 534. M.C.Y. Niu, p 459.
Cantrell, C.D. Modern Mathematical Methods for Physicists and Bramwell’s Helicopter Dynamics — second edition. A.R.S.
Engineers, p 295. Bramwell, G. Done and D. Balmford, p 534.
Cercignani, C. Rarefied Gas Dynamics: From Basic Concepts to Classical Mechanics: A Modern Introduction. M.W. McCall, p 607.
Actual Calculations, p 231. Composite Airframe Structures: Practical Design Information and
Chapman, C.J. High Speed Flow: Cambridge Texts in Applied Data. M.C.Y. Niu, p 459.
Mathematics Series, p 230. Computational Mesh Adaptation: ECARP — European Computational
Dole, C.E. and Lewis, J.E. Flight Theory and Aerodynamics: A Aerodynamics Research Project. D.P. Hills et al (Ed), p 230.
Practical Guide for Operational Safety — second edition, p 96. EW1OlI: A First Course in Electronic Warfare. D. Adamy, p 684.
Finite Element Modelling of Composite Materials and Structures.
Durbin, P.A. and Petterson Reif, B.A. Statistical Theory and Modelling
F.L. Matthews et al. p 160.
for Turbulent Flows, p 295.
Finite Element Multidisciplinary Analysis. K.K. Gupta and J.L.
Gad-el-Hak, M. Flow Control: Passive. Active and Reactive Flow
Meek, p 231.
Management, p 150.
Flexible Multibody Dynamics: A Finite Element Approach. M.
Galdi, G.P. et ai (Eds) Fundamental Directions in Mathematical Fluid
Geradin and A. Cardona, p 400.
Mechanics, p 632.
Flight Theory and Aerodynamics: A Practical Guide for Operational
Geradin, M. and Cardona, A. Flexible Multibody Dynamics: A Finite
Satety — second edition. C.E. Dole and J.E. Lewis, p 96.
Element Approach, p 400.
Flow Control: Passive, Active and Reactive Flow Management. M.
Ginsberg. J.H. Mechanical and Structural Vibrations: Theory and
Gad-el-Hak, p 150.
Applications, pp 534 and 550.
Fundamental Directions in Mathematical Fluid Mechanics. G.P. Galdi
Gupta, K.K. and Meek, J.L. Finite Element Multidisciplinary Analysis,
et al (Eds), p 632.
p 231.
Fundamentals of Kalman Filtering: A Practical Approach. Progress
Hills, D.P. et al (Ed) Computational Mesh Adaptation: ECARP —
in Astronautics and Aeronautics series Vol 190. P. Zarchan and H.
European Computational Aerodynamics Research Project, p 230.
Musoff, p 400.
Howe, D. Aircraft Conceptual Design Synthesis, p 160.
High Speed Flow: Cambridge Texts in Applied Mathematics Series.
Katz, J. and Plotkin, A. Low-Speed Aerodynamics — second edition,
C.J. Chapman, p 230.
p 550.
Introduction to Interactive Boundary Layer Theory. [.J. Sobey, p 294.
Lacomme, P. ef al Air and Spaceborne Radar Systems: An Introduction,
Low-Speed Aerodynamics — second edition. J. Katz and A. Plotkin,
p 684.
p 550.
Matthews, F.L. ef a! Finite Element Modelling of Composite Materials
Mathematical Methods with Applications. M. Rahman, p 684.
and Structures, p 160. Mechanical and Structural Vibrations: Theory and Applications. J.H.
MeCall, M.W. Classical Mechanics: A Modern Introduction, p 607. Ginsberg, pp 534 and 550.
Megson, T.H.G. Aircraft Structures for Engineering Students — Micropropulsion for Small Spacecraft. Progress in Astronautics and
third edition, p 607. Aeronautics Series, Vol 187. M.M. Micci and A.D. Ketsdever
Micci, M.M. and Ketsdever, A.D. (Eds) Micropropulsion tor Small (Eds), p 400.
Spacecraft: Progress in Astronautics and Aeronautics Series, Vol Modeiling and Simulation of Aerospace Vehicle Dynamics. P.H.
187, p 400. Zipfel, p 294.
Niu, M.C.Y. Airframe Structural Design: Practical Design Information Modern Mathematical Methods for Physicists and Engineers. C.D.
and Data, p 459. Cantrell, p 295.
Niu, M.C.Y. Composite Airframe Structures: Practical Design Infor- Optimal Control. Systems and Control: Foundations and Applications
mation and Data, p 459. Series. R. Vinter, p 230.
Noor, A.K. (Ed) Structures Technology for Future Aerospace Systems. Principles of Optimal Design: Modeling and Computation. P.Y.
Progress in Astronautics and Aeronautics Series, Vol 188, p 96. Papalambros and D.J. Wilde, pp 458-459.
Papalambros, P.Y. and Wilde, D.J. Principles of Optimal Design: Rarefied Gas Dynamics: From Basic Concepts to Actual Calculations.
Modeling and Computation, pp 458-459. C. Cercignani, p 231.
Rahman, M. Mathematical Methods with Applications, p 684. Smart Structures: Analysis and Design. A.V. Srinivasan and D.M.
Saatdjian, E. Transport Phenomena: Equations and Numerical Solu- McFarland, p 458.
tions, p 632. Some Fundamentals on the Performance of Ramjets with Subsonic
Sobey, L.J. Introduction to Interactive Boundary Layer Theory, p 294. and Supersonic Combustion. H. Wittenberg, p 96.
Srinivasan, A.V. and McFarland, D.M. Smart Structures: Analysis Statistical Theory and Modelling for Turbulent Flows. B.A. Petter-
and Design, p 458. son Reif and P.A. Durbin, p 295.
Taylor J.D. (Ed) Ultra-Wideband Radar Technology, p 295. Structures Technology for Future Aerospace Systems. Progress in
Vinter, R. Optimal Control. Systems and Control: Foundations and Astronautics and Aeronautics Series, Vol 188. A.K. Noor (Ed), p 96.
Applications series, p 230. Transport Phenomena: Equations and Numerical Solutions. E. Saatd-
Wittenberg, H. Some Fundamentals on the Performance of Ramjets jian, p 632.
with Subsonic and Supersonic Combustion, p 96. Ultra-Wideband Radar Technology. J.D. Taylor (Ed), p 295.
708 THE AERONAUTICAL JOURNAI DECEMBER 2001
COMMERCIAL AVIATION Errata: A strategic review of the large civil aeroengine market and
On (civil) aviation future(s). D.M. Bushnell, pp 603-606 the paradigm shift to a service-oriented environment. C.I.V. Kerr
and P.C. Ivey, p 343.
COMPUTATIONAL FLUID DYNAMICS Future challenges for powerplant aerodynamic integration in combat
Embedded direct numerical simulation for aeronautical CFD. N.D. aircraft. M.G. Philpot, pp 335-342.
Sandham, M. Alam and S. Morin, pp 193-198. Impacts of aero-engine deteriorations on military aircraft mission’s
effectiveness. M. Naeem, R. Singh and D. Probert, pp 685-695.
DEFENCE Life extending controller design for reusable rocket engines. A. Ray.
Impacts of aero-engine deteriorations on military aircraft mission's M.S. Holmes and C.F. Lorenzo, pp 315-322.
effectiveness. M. Naeem, R. Singh and D. Probert, pp 685-695 Optimisation of aero gas turbine engines. A. Guha, pp 345-358.
Performance parameter benchmarks for small piston aero-engines.
DYNAMICS B.J Brinkworth, pp 63-68.
An investigation of Handley Page Jetstream handling during landing. Saving costs in design, manufacturing and operation of aero engine
G.J. Mullen, pp 307-314. parts. J. Broede, pp 619-626.
Fuzzy modelling for aircraft dynamics identification. G. Mengali, pp Simulation of flows within an electrostatic ion thruster for space
551-555. missions. M. Jugroot and J.K. Harvey. pp 613-618.
The design of fly-by-wire flight control systems. C. Fielding, pp
RESEARCH MANAGEMENT
543-549.
\ strategic European approach to aerodynamics research, technology
and development. P.C. Dexter, pp 451-457.
The application of Pareto methods to multidisciplinary design opti-
ROTORCRAFT
misation. J.C. Harris and S.V. Fenwick, pp 329-334
Helicopter encounters with aircraft vortex wakes. G.D. Padfield and
G.P. Turner, pp 1-8.
ERRATA
Laplace-domain approximation to the transfer functions of a rotor
Errata: A strategic review of the large civil aeroengine market and
blade in forward flight. F. Nitzsche, pp 233-240.
the paradigm shift to a service-oriented environment. C.1.V. Kerr
Multigrid acceleration of an upwind Euler method for hovering rotor
and P.C. Ivey, p 343. flows. C.B. Allen, pp 517-524.
Errata: Inflight icing data gathering during routine flight operations Non-inertial multiblock Navier-Stokes calculation for hovering rotor
—acase study. A.P. Brown, p 642. flowfields using relative velocity approach. B. Zhong and N. Qin,
Errata: Planning for super safety: the fail-safe dimension. R.W. pp 3~ 79-389
Howard, p 286. Performance enhancement evaluation of an actuated trailing edge
flap. W. Chan and A. Brocklehurst, pp 391-399.
FLIGHT TESTING Trajectory tracking for a helicopter model. G. Avanzini, pp 69-76.
Errata: Inflight icing data gathering during routine flight operations
a case study. A.P. Brown, p 642. RUNWAY DEBRIS
Inflight icing data gathering during routine flight operations Characterisation of the realistic impact threat from runway debris.
case study. A.P. Brown, pp 501-516. E.S. Greenhalgh, G.A.F. Chichester, A. Mew. M. Slade and R.
Integrated air data sensors. M.A. Menzies, pp 2234- 229. Bowen, pp 557-570.
INTERNAL BALLISTICS SAFETY
A new moving-boundary algorithm with application to SRM internal Errata: Planning for super safety: the fail-safe dimension. R.W.
ballistics. S.M.H. Karimian and A. Amoli, pp 697-705 Howard, p 286
Simulating the evacuation of a commercial airliner. C.R. Robbins
KITES and S. McKee, pp 323-328.
Kite equilibrium and bridle length. K. Alexander and J. Stevenson,
SIMULATION
pp 535-541.
\eroservoelastic simulation by time-marching. L. Djayapertapa and
C.B. Allen, pp 667-678.
MISSILES
Simulating the evacuation of a commercial airliner. C.R. Robbins
Air-to-ground weapon aiming — a synopsis and a look to the future.
and S. McKee, pp 323-328.
K.L. Edwards, S.J. Lloyd and J.F. Ralph, pp 53-62.
Simulation of flows within an electrostatic ion thruster for space
Hypersonic missiles some problem areas. R.A. East and J.A.
missions. M. Jugroot and J.K. Harvey, pp 613-618.
Edwards, pp 643-651.
SYSTEMS
NOISE Air-to-ground weapon aiming — a synopsis and a look to the future.
Active control of fan noise from high-bypass ratio aeroengines: a K.L. Edwards, S.J. Lloyd and J.F. Ralph, pp 53-62.
numerical study. P. Traub, F. Kennepohl and K. Heinig, pp 627-631. An all weather millimetre wave imaging radar for UAVs. A. Britton
Effect of Mach number on the acoustic field of 2:1 elliptic-slot jet. E. and D. Joynson, pp 609-612.
Rathakrishnan and S.B. Verma, pp 9-16. A neural network approach to the calibration of a flush air data system.
Experimental study on the flow and noise characteristics of under- W.J. Crowther and P.J. Lamont, pp 85-95.
expanded notched slot jets. S.B. Verma and E. Rathakrishnan, pp Applications of multirate optical fibre code-division-multiplexing
267-275. systems to high-speed data communications for air traffic control.
A.B. Sharma and J-G. Jian-Guo Zhang, pp 33-39.
PROPULSION A technique for predicting pilot model parameters using inverse
Active control of fan noise from high-bypass ratio aeroengines: a simulation. G.R. Leacock and D.G. Thomson, pp 97-103.
numerical study. P. Traub, F. Kennepohl and K. Heinig, pp 627-631. Avionics extrapolations (A foray into the future of avionics). R. Fitz-
A strategic review of the large civil aeroengine market and the para- Patrick, pp 241-253.
digm shift to a service-oriented environment. C.I.V. Kerr and P.C. Energy requirements for the flight of micro air vehicles. J.F. Henderson,
Ivey, pp 287-293. G.D. Lock and M.I. Woods, pp 135-149.
INDEX TO VOLUME 105 709
Integrated air data sensors. M.A. Menzies, pp 223-229. supersonic wind tunnel. J. Weiss, H. Knauss, S. Wagner and A.D.
Integrated sensor/actuator FDI and reconfigurable control for fault- Kosinov, pp 435-441.
tolerant flight control system design. Ch.M. Hajiyev and F. Experimental and numerical investigation of wind tunnel wall inter-
ference near Mach one. M. Mokry, M. Khalid, Y. Mébarki and A.
Life extending controller design for reusable rocket engines. A. Ray, Rebaine, pp 589-596.
M.S. Holmes and C.F. Lorenzo, pp 315-322. Extensions to Maskell’s theory for blockage effects on bluff bodies
Numerical and experimental investigations on the reduction of wind in a closed wind tunnel. J.E. Hackett and K.R. Cooper, pp 409-
tunnel wall interference by means of adaptive slots. O. Meyer, W. 418.
Nitsche and I. Futterer, pp 571-580. Numerical and experimental investigations on the reduction of wind
Numerical studies of infrared signature levels of complete aircraft. tunnel wall interference by means of adaptive slots. O.M eyer, W.
S.P. Mahilikar, S.K. Sane, U.N. Gaitonde and A.G. Marathe, pp Nitsche and I. Futterer, pp 571-580.
185-192.
The accuracy of internal wind tunnel balances for wind tunnel force
The application of self-organising fuzzy control to station-keeping in
measurements, the problem of definition and verification. B.
unmanned air vehicles. J.T. Platts and W. Forsythe, pp 359-370.
Ewald, pp 443-449.
The design of fly-by-wire flight control systems. C. Fielding, pp
543-549.
UNMANNED AIR VEHICLES (UAVs)
Theoretical and experimental investigations on an active control system
An all weather millimetre wave imaging radar for UAVs. A. Britton
for vertical fin buffeting alleviation using strain actuation. F.
and D. Joynson, pp 609-612.
Nitzsche, S. Liberatore and D.G. Zimcik, pp 277-285.
Energy requirements for the flight of micro air vehicles. J.F. Hender-
Trajectory tracking for a helicopter model. G. Avanzini, pp 69-76.
son, G.D. Lock and M.1. Woods, pp 135-149.
TESTING FACILITIES AND TECHNIQUES The application of self-organising fuzzy control to station-keeping in
Constant temperature hot-wire measurements in a short duration unmanned air vehicles. J.T. Platts and W. Forsythe, pp 359-370.
Author Index
ALAM, M., MORIN, S. and SANDHAM, N.D. BOWEN, R., GREENHALGH, E.S., CHICHESTER, G.A.F.,
Embedded direct numerical simulation for aeronautical CFD, pp MEW, A. and SLADE, M.
193-198. Characterisation of the realistic impact threat from runway debris, pp
557-570.
ALEXANDER, K. and STEVENSON, J.
Kite equilibrium and bridle length, pp 535-541. BRAY, D., KNOWLES, K. and TABORDA, N.
Experimental investigation into transonic flows over tandem cavities,
ALLEN, C.B. pp 119-124.
Multigrid acceleration of an upwind Euler method for hovering rotor
flows, pp 517-524. BREARD, C., BARAKOS, G., VAHDATI, M., SAYMA, A.L.
and IMREGUN, M.
ALLEN, C.B. and DJAYAPERTAPA, L. A fully distributed unstructured Navier-Stokes solver for large-scale
Aeroservoelastic simulation by time-marching, pp 667-678. aeroelasticity computations, pp 419-426.
ALLEN, J.E., EVANGELOU, L.D., SELF, A.W. and LO, S. BRINKWORTH, BJ.
Trimmed deep stall on the F-16 Fighting Falcon, pp 679-683. Performance parameter benchmarks for small piston aero-engines,
pp 63-68.
AMOLI, A. and KARIMIAN, S.M.H.
BRITTON, A. and JOYNSON, D.
A new moving-boundary algorithm with application to SRM internal
An all weather millimetre wave imaging radar for UAVs, pp 609-612.
ballistics, pp 697-705.
BROCKLEHURST, A. and CHAN, W.
AVANZINI, G.
Performance enhancement evaluation of an actuated trailing edge
Trajectory tracking for a helicopter model, pp 69-76.
flap, pp 391-399.
BADCOCK, K.J., RICHARDS, B.E. and HENDERSON, J. BROEDE, J.
Understanding subsonic and transonic cavity flows, pp 77-84. Saving costs in design, manufacturing and operation of aero engine
parts, pp 619-626.
BADCOCK, K.J., WOODGATE, M.A., RICHARDS, B.E. and
GOUBA, G.S.L. BROWN, A.P.
Implicit method for the time marching analysis of flutter, pp 199-214. Inflight icing data gathering during routine flight operations — a
A data exchange method for fluid-structure interaction problems, pp case study, pp 501-516.
215-221. Errata: Inflight icing data gathering during routine flight operations
— acase study, p 642.
BARAKOS, G., VAHDATI, M., SAYMA, A.L, BREARD, C.
and IMREGUN, M. BUSHNELL, D.M.
A fully distribuied unstructured Navier-Stokes solver for large-scale On (civil) aviation future(s), pp 603-606.
aeroelasticity computations, pp 419-426.
CALISKAN, F. and HAJIYEV, CH.M.
BATTEN, P., CRAFT, T.J. and LESCHZINER, M.A. Integrated sensor/actuator FDI and reconfigurable control for fault-
Reynolds-stress modelling of afterbody flows, pp 297-306. tolerant flight control system design, pp
710 THE AERONAL rICAL JOURNAI DECEMBER 2001
CHAN, W. and BROCKLEHURST, A. FITZPATRICK, R.
Performance enhancement evaluation of an actuated trailing edge \vionics extrapolations (A foray into the future of avionics), pp 241-
flap. pp 391-399. Pin
CHICHESTER, G.A.F., GREENHALGH, E.S., MEW, A., FORSYTHE, W. and PLATTS, J.T.
SLADE, M. and BOWEN, R. The application of self-organising fuzzy control to station-keeping in
Characterisation of the realistic impact threat from runway debris. pp unmanned air vehicles, pp 359-370.
557-570
FUTTERER, L., MEYER, O. and NITSCHE, W.
CHILDS, M., HUNT, D.L. and MAINA, M. Numerical and experimental investigations on the reduction of wind
QUACC, a novel method for predicting unsteady flows including tunnel wall interference by means of adaptive slots, pp 571-580.
propellers and store release, pp 427-434.
GAITONDE, U.N., MARATHE, A.G., MAHILIKAR, S.P. and
COBBIN, A.M., WONG, P.W.C. and MAINA, M. SANE, S.K.
Transition and separation control in the leading edge region, pp 37 Numerical studies of infrared signature levels of complete aircraft,
3/8. pp 185-192.
COOPER, K.R. and HACKETT, J.E.
GALBRAITH, R.A.McD., GREEN, R.B. and COTON, F.N.
Extensions to Maskell’s theory for blockage effects on bluff bodies
Phe effect of wing planform shape on dynamic stall, pp 151-159.
in a closed wind tunnel, pp 409-418.
GOURA, G.S.L., BADCOCK, K.J., WOODGATE, M.A. and
COTON, F.N., GALBRAITH, R.A.McD. and GREEN, R.B.
RICHARDS, B.E.
The effect of wing planform shape on dynamic stall, pp 151-159
Implicit method for the time marching analysis of flutter, pp 199-214.
\ data exchange method for fluid-structure interaction problems, pp
CRAFT, T.J., LESCHZINER, M.A. and BATTEN, P.
215-221.
Reynolds-stress modelling of afterbody flows. pp 297-306
GRAHAM, W.R.
CROWTHER, W.J. and LAMONT, P.J.
\ neural network approach to the calibration of a flush air data system, An assessment of the 2D vortex method in aircraft wake simulation,
pp 85-95. pp 653-666
CZECH, M., MAURIDES, T., SAVORY, E. and TOY, N. GREEN, R.B., COTON, F.N. and GALBRAITH, R.A.McD.
Flow regimes associated with yawed rectangular cavities, pp 125-134. Phe effect of wing plantorm shape on dynamic stall, pp 151-159.
DEXTER, P.C. GREENHALGH, E.S., CHICHESTER, G.A.F., MEW, A.,
\ strategic European approach to aerodynamics research, technology SLADE, M. and BOWEN, R.
and development, pp 451-457 Characterisation of the realistic impact threat from runway debris, pp
557-570.
DJAYAPERTAPA, L. and ALLEN, C.B.
Aeroservoelastic simulation by time-marching. pp 667-678 GUHA, A.
Optimisation of aero gas turbine engines, pp 345-358
EAST, R.A. and EDWARDS, J.A.
Hypersonic missiles some problem areas. pp 643-651 HACKETT, J.E. and COOPER, K.R.
Extensions to Maskell’s theory for blockage effects on blutf bodies
EDWARDS, J.A. and EAST, R.A. in a closed wind tunnel, pp 409-418.
Hypersonic missiles — some problem areas. pp 643-651
HAJIYEV, CH.M. aad CALISKAN, F.
EDWARDS, K.L. LLOYD, S.J. and RALPH, J.F. Integrated sensor/actuator FDI and reconfigurable control for fault-
Air-to-ground weapon aiming — a synopsis and a look to the future. tolerant flight control system design, pp 525-533.
pp 53-62
HARRIS, J.C. and FENWICK, S.V.
EVANGELOU, L.D., ALLEN, J.E., SELF, A.W. and LO, S. The application of Pareto methods to multidisciplinary design opti-
rrimmed deep stall on the F-16 Fighting Falcon, pp 679-683. misation, pp 329-334.
EWALD, B. HARVEY, J.K. and JUGROOT, M.
Phe accuracy of internal wind tunnel balances for wind tunnel force Simulation of flows within an electrostatic ion thruster for space
measurements, the problem of definition and verification, pp 443- missions, pp 613-618.
449.
HASAN, R.G.M. and McGUIRK, J.J.
FENWICK, S.V. and HARRIS, J.C. Assessment of turbulence model performance for transonic flow
The application of Pareto methods to multidisciplinary design over an axisymmetric bump, pp 17-31.
optimisation, pp 329-334.
HE, L. and ZHENG, Y.
FIELDING, C. Multigrid upwind Euler/Navier-Stokes computation on adaptive
The desigs n of flyy--b)b y-wire fligg ht control sy) stems. PpIp 543-549. unstructured meshes, pp 173-184.
FIELDING, J.P. and YOUNG, T.M. HEINIG, K., TRAUB, P. and KENNEPOHL, F.
Potential fuel savings due to hybrid laminar flow control under oper- Active control of fan noise from high-bypass ratio aeroengines: a
ational conditions, pp 581-588. numerical study, pp 627-631.
INDEX TO VOLUME 105 711
HENDERSON, J., BADCOCK, K.J. and RICHARDS, B.E. KNAUSS, H., WEISS, J., WAGNER, S. and KOSINOV, A.D.
Understanding subsonic and transonic cavity flows, pp 77-84. Constant temperature hot-wire measurements in a short duration
supersonic wind tunnel, pp 435-441.
HENDERSON, J.F., LOCK, G.D. and WOODS, M.I.
Energy requirements for the flight of micro air vehicles, pp 135-149. KNOWLES, K., TABORDA, N. and BRAY, D.
Experimental investigation into transonic flows over tandem cavities,
HENRY, F.S. and KUPPER, C. pp 119-124.
A numerical study of the application of vane and air-jet vortex
generators, pp 255-265. KOSINOV, A.D., KNAUSS, H., WEISS, J. and WAGNER, S.
Constant temperature hot-wire measurements in a short duration
HENRY, F.S., LEWINGTON, N.P., PEAKE, D.J. and SINGH, C. supersonic wind tunnel, pp 435-441.
Numerical and experimental investigations of air-jet vortex generators
in streamwise pressure gradients, pp 401-407.
KUPPER, C. and HENRY, F.S.
A numerical study of the application of vane and air-jet vortex
HOLMES, M.S., LORENZO, C.F. and RAY, A.
generators, pp 255-265.
Life extending controller design for reusable rocket engines, pp 315-
Baz.
LAMONT, P.J. and CROWTHER, W.J.
A neural network approach to the calibration of a flush air data system,
HONG, G., MALLINSON, S.G. and REIZES, J.A.
pp 85-95.
An experimental and numerical study of synthetic jet flow, pp 41-49.
HOWARD, R.W. LEACOCK, G.R. and THOMSON, D.G.
Errata: Planning for super safety: the fail-safe dimension, p 286. A technique for predicting pilot model parameters using inverse
simulation, pp 97-103.
HUNT, D.L.
Development and application of farfield drag extraction techniques LESCHZINER, M.A., BATTEN, P. and CRAFT, T.J.
for complex viscous flows, pp 161-169. Reynolds-stress modelling of afterbody flows, pp 297-306
HUNT, D.L., CHILDS, M. and MAINA, M. LEWINGTON, N.P., HENRY, F.S., PEAKE, D.J. and SINGH, C.
QUACC, a novel method for predicting unsteady flows — including Numerical and experimental investigations of air-jet vortex genera-
propellers and store release, pp 427-434. tors in streamwise pressure gradients, pp 401-407.
IMREGUN, M., BREARD, C., BARAKOS, G., VAHDATI, M., LIBERATORE, S., ZIMCIK, D.G. and NITZSCHE, F.
and SAYMA, A.L. Theoretical and experimental investigations on an active control system
A fully distributed unstructured Navier-Stokes solver for large-scale for vertical fin buffeting alleviation using strain actuation, pp 277-
aeroelasticity computations, pp 419-426. 285.
IVEY, P.C. and KERR, C.LV. LLOYD, S.J., RALPH, J.F. and EDWARDS, K.L.
A strategic review of the large civil aeroengine market and the para- Air-to-ground weapon aiming — a synopsis and a look to the future,
digm shift to a service-oriented environment, pp 287-293. pp 53-62.
Errata: A strategic review of the large civil aeroengine market and
the paradigm shift to a service-oriented environment, p 343. LO, S., ALLEN, J.E., EVANGELOU, L.D. and SELF, A.W.
Trimmed deep stall on the F-16 Fighting Falcon, pp 679-683.
JOYNSON, D. and BRITTON, A.
An all weather millimetre wave imaging radar for UAVs, pp 609-912. LOCK, G.D., WOODS, M.I. and HENDERSON, J.F.
Energy requirements for the flight of micro air vehicles, pp 135-149.
JUGROOT, M. and HARVEY, J.K.
Simulation of flows within an electrostatic ion thruster for space LORENZO, C.F., RAY, A. and HOLMES, MLS.
missions, pp 613-618. Life extending controller design for reusable rocket engines, pp 315-
322.
JUPP, J.
Wing aerodynamics and the science of compromise, pp 633-641. McGUIRK, J.J. and HASAN, R.G.M.
Assessment of turbulence model performance for transonic flow
KARIMIAN, S.M.H. and AMOLI, A. over an axisymmetric bump, pp 17-31.
A new moving-boundary algorithm with application to SRM internal
bailistics, pp 697-705. McKEE, S. and ROBBINS, C.R.
Simulating the evacuation of a commercial airliner, pp 323-328.
KENNEPOHL, F., TRAUB, P. and HEINIG, K.
Active control of fan noise from high-bypass ratio aeroengines: a MAHILIKAR, S.P., SANE, S.K., GAITONDE, U.N. and
numerical study, pp 627-631. MARATHE, A.G.
Numerical studies of infrared signature levels of compiete aircraft,
KERR, C.LV. and IVEY, P.C. pp 185-192.
A strategic review of the large civil aeroengine market and the para-
digm shift to a service-oriented environment, pp 287-293. MAINA, M., CHILDS, M. and HUNT, D.L.
Errata: A strategic review of the large civil aeroengine market and QUACC, a novel method for predicting unsteady flows — including
the paradigm shift to a service-oriented environment, p 343. propellers and store release, pp 427-434.
KHALID, M., MOKRY, M., MEBARKI, Y. and REBAINE, A. MAINA, M., COBBIN, A.M. and WONG, P.W.C.
Experimental and numerical investigation of wind tunnel wall inter- Transition and separation control in the leading edge region, nn 371-
ference near Mach one, pp 589-596. 378.
viz THE AERONAUTICAL JOURNAL DECEMBER 2001
MALLINSON, S.G., REIZES, J.A. and HONG, G. PHILPOT, M.G.
An experimental and numerical study of synthetic jet flow, pp 41-49. Future challenges for powerplant aerodynamic integration in combat
aircraft, pp 335-342.
MARATHE, A.G., MAHILIKAR, S.P., SANE, S.K. and
GAITONDE, U.N. PLATTS, J.T. and FORSYTHE, W.
Numerical studies of infrared signature levels of complete aircraft. The application of self-organising fuzzy control to station-keeping in
pp 185-192. unmanned air vehicles, pp 359-370.
MAURIDES, T., SAVORY, E., TOY, N. and CZECH, M. PROBERT, D., NAEEM, M. and SINGH, R.
Flow regimes associated with yawed rectangular cavities, pp 125-134. Impacts of aero-engine deteriorations on military aircraft mission’s
effectiveness, pp 685-695.
MEBARKI, Y., MOKRY, M., KHALID, M. and REBAINE, A.
Experimental and numerical investigation of wind tunnel wall inter- QIN, N. and RICHARDSON, G.
ference near Mach one. pp 589-596. \n eddy-viscosity limited algebraic stress model for shock—boundary-
layer interaction, pp 105-118.
MENGALT, G.
Fuzzy modelling for aircraft dynamics identification, pp 551-555. QIN, N. and ZHONG, B.
Non-inertial multiblock Navier-Stokes calculation for hovering rotor
MENZIES, M.A. flowfields using relative velocity approach, pp 379-389.
Integrated air data sensors, pp 223-229.
RALPH, J.F., EDWARDS, K.L. and LLOYD, S.J.
MEW, A., GREENHALGH, E.S., CHICHESTER, G.A.F., Air-to-ground weapon aiming — a synopsis and a look to the future,
SLADE, M. and BOWEN, R. pp 53-62.
Characterisation of the realistic impact threat from runway debris. pp
557-570. RATHAKRISHNAN, E. and VERMA, S.B.
Effect of Mach number on the acoustic field of 2:1 elliptic-slot jet,
MEYER, O., NITSCHE, W. and FUTTERER, I. pp 9-16.
Numerical and experimental investigations on the reduction of wind Experimental study on the flow and noise characteristics of under-
tunnel wall interference by means of adaptive slots, pp 571-580. expanded notched slot jets, pp 267-275.
MOKRY, M., KHALID, M., MEBARKI, Y. and REBAINE, A. RAY, A., HOLMES, M.S. and LORENZO, C.F.
Experimental and numerical investigation of wind tunnel wall inter- Life extending controller design for reusable rocket engines. pp 315-
ference near Mach one, pp 589-596. 37).
MORIN, S., SANDHAM, N.D. and ALAM, M. REBAINE, A., MOKRY, M., KHALID, M. and MEBARKL, Y.
Embedded direct numerical simulation for aeronautical CFD. pp Experimental and numerical investigation of wind tunnel wall inter-
193-198. ference near Mach one, pp 589-596.
MULLEN, G.J. REIZES, J.A., HONG, G. and MALLINSON, S.G.
An investigation of Handley Page Jetstream handling during landing, An experimental and numerical study of synthetic jet flow, pp 41-49.
pp 307-314.
RICHARDS, B.E., GOURA, G.S.L., BADCOCK, K.J. and
NAEEM, M., SINGH, R. and PROBERT, D.
WOODGATE, M.A.
Impacts of aero-engine deteriorations on military aircraft mission's
Implicit method for the time marching analysis of flutter, pp 199-214.
effectiveness, pp 685-695.
\ data exchange method for fluid-structure interaction problems, pp
215-221.
NITZSCHE, F.
Laplace-domain approximation to the transfer functions of a rotor
RICHARDS, B.E., HENDERSON, J. and BADCOCK, K.J.
blade in forward flight, pp 233-240.
Understanding subsonic and transonic cavity flows, pp 77-84.
NITZSCHE, F., LIBERATORE, S. and ZIMCIK, D.G.
RICHARDSON, G. and QIN, N.
Theoretical and experimental investigations on an active control system
\n eddy-viscosity limited algebraic stress model for shock—boundary-
for vertical fin buffeting alleviation using strain actuation, pp 277-
layer interaction, pp 105-118.
285.
NITSCHE, W., MEYER, O. and FUTTERER, I. ROBBINS, C.R. and MCKEE, S.
Numerical and experimental investigations on the reduction of wind Simulating the evacuation of a commercial airliner, pp 323-328.
tunnel wall interference by means of adaptive slots, pp 571-580.
SANDHAM, N.D., ALAM, M. and MORIN, S.
O’BRIEN, S. and ZHONG, S. Embedded direct numerical simulation for aeronautical CFD, pp
Visualisation of flow separation with shear-sensitive liquid crystals, 193-198.
pp 597-602.
SANE S.K., GAITONDE U.N., MARATHE A.G. and MAHI-
PADFIELD, G.D. and TURNER, G.P. LIKAR, S.P.
Helicopter encounters with aircraft vortex wakes, pp 1-8 Numerical studies of infrared signature levels of complete aircraft,
pp 185-192.
PEAKE, D.J., LEWINGTON, N.P., HENRY, F.S. and SINGH, C.
Numerical and experimental investigations of air-jet vortex generators SAVORY, E., TOY, N., CZECH, M. and MAURIDES, T.
in streamwise pressure gradients. pp 401-407. Flow regimes associated with yawed rectangular cavities, pp 125-134.
INDEX TO VOLUME 105
SAYMA, A.L, BREARD, C., BARAKOS, G., VAHDATI, M., VERMA, S.B. and RATHAKRISHNAN, E.
and IMREGUN, M. Effect of Mach number on the acoustic field of 2:1 elliptic-slot jet.
A fully distributed unstructured Navier-Stokes solver for large-scale pp 9-16.
aeroelasticity computations, pp 419-426. Experimental study on the flow and noise characteristics of under-
expanded notched slot jets, pp 267-275.
SELF, A.W., ALLEN, J.E., EVANGELOU, L.D. and LO, S.
Trimmed deep stall on the F-16 Fighting Falcon, pp 679-683. WAGNER, S., KNAUSS, H., WEISS, J. and KOSINOV, A.D.
Constant temperature hot-wire measurements in a short duration
SHARMA, A.B. and ZHANG, J-G. supersonic wind tunnel, pp 435-441.
Applications of multirate optical fibre code-division-multiplexing
systems to high-speed data communications for air traffic control, WEISS, J., KNAUSS, H., WAGNER, S. and KOSINOV, A.D.
pp 33-39. Constant temperature hot-wire measurements in a short duration
supersonic wind tunnel, pp 435-441.
SINGH, C., LEWINGTON, N.P., HENRY, F.S. and PEAKE, D.J.
Numerical and experimental investigations of air-jet vortex generators WONG, P.W.C., COBBIN, A.M. and MAINA, M.
in streamwise pressure gradients, pp 401-407. Transition and separation control in the leading edge region. pp 371-
378.
SINGH, R., NAEEM, M. and PROBERT, D.
Impacts of aero-engine deteriorations on military aircraft mission's WOODGATE, M.A., RICHARDS, B.E., GOURA, G.S.L. and
BADCOCK, K.J.
effectiveness. pp 685-695.
Implicit method for the time marching analysis of flutter, pp 199-214.
A data exchange method for fluid-structure interaction problems, pp
SLADE, M., GREENHALGH, E.S., CHICHESTER, G.A.F.,
215-221.
MEV, A. and BOWEN, R.
Characterisation of the realistic impact threat from runway debris, pp
WOODS, M.I., HENDERSON, J.F. and LOCK, G.D.
557-570.
Energy requirements for the flight of micro air vehicles, pp 135-149.
STEVENSON, J. and ALEXANDER, K.
YOUNG, T.M. and FIELDING, J.P.
Kite equilibrium and bridle length, pp 535-541.
Potential fuel savings due to hybrid laminar flow control under oper-
ational conditions, pp 581-588.
TABORDA, N., BRAY, D. and KNOWLES, K.
Experimental investigation into transonic flows over tandem cavities, ZHANG, J-G. and SHARMA, A.B.
pp 119-124. Applications of multirate optical fibre code-division-multiplexing
systems to high-speed data communications for air traffic control,
THOMSON, D.G. and LEACOCK, G.R. pp 33-39.
A technique for predicting pilot model parameters using inverse
simulation, pp 97-103. ZHENG, Y. and HE, L.
Multigrid upwind Euler/Navier-Stokes computation on adaptive
TOY, N., CZECH, M., MAURIDES, T. and SAVORY, E. unstructured meshes, pp 173-184.
Flow regimes associated with yawed rectangular cavities, pp 125-134.
ZHONG, B. and QIN, N.
TRAUB, P., KENNEPOHL, F. and HEINIG, K. Non-inertial multiblock Navier-Stokes calculation for hovering rotor
Active control of fan noise from high-bypass ratio aeroengines: a flowfields using relative velocity approach, pp 379-389.
numerical study, pp 627-631.
ZHONG, S. and O'BRIEN, S.
TURNER, G.P. and PADFIELD, G.D. Visualisation of flow separation with shear-sensitive liquid crystals,
Helicopter encounters with aircraft vortex wakes, pp 1-8. pp 597-602.
VAHDATI, M., BREARD, C., BARAKOS, G., SAYMA, A.L. ZIMCIK, D.G., NITZSCHE, F. and LIBERATORE, S.
and IMREGUN, M. Theoretical and experimental investigations on an active control system
A fully distributed unstructured Navier-Stokes solver for large-scale for vertical fin buffeting alleviation using strain actuation, pp 277-
aeroelasticity computations, pp 419-426. 285.
Volume CV
Number 1043 January pp I-51
Number 1044 February pp 53-103
Number 1045 March pp 105-171
Number 1046 April pp 173-231
Number 1047 May pp 233-295
Number 1048 June pp 297-343
Number 1049 July pp 345-407
Number 1050 August pp 409-459
Number 1051 September pp 501-555
Number 1052 October pp 557-607
Number 1053 November pp 609-65 |
Number 1054 December pp 653-715