DECEMBER 2010

INDEX TO VOLUME 114

THE AERONAUTICAL JOURNAL

OF THE ROYAL AERONAUTICAL SOCIETY

Volume CXIV

January-December 2010

Subject Index

ACOUSTICS

Optimisation of RNAV noise and emission abatement standard instrument departures. S. Hartjes, H.G. Visser and S.J. Hebly, pp 757-767.

The effect of gravity on a shaped sonic boom. T. Cain, pp 651- 656.

AERODYNAMICS

A comprehensive numerical study of battle damage and repairs

upon the aerodynamic characteristics of an aerofoil. M. Saeedi,

F. Ajalli and M. Mani, pp 469-484.

A hybrid frequency-time domain technique for ground effect identification. A. Vitale, N. Genito, L. Garbarino, U. Ciniglio and F. Corraro, pp 377-385.

Aerodynamic study of corrugated skins for morphing wing applications. C. Thill, J.D. Downsborough, S.J. Lai, I.P. Bond and D.P. Jones, pp 237-244.

Aerodynamics A discipline swept away? C.-C. Rossow, pp 599-609.

Development and validation of an efficient direct numerical optimisation approach for aerofoil shape design. M. Khurana and H. Winarto, pp 611-628.

Drag reduction on a spiked body at hypersonic speed. G. d’Humieres, J.L. Stollery, pp 113-119.

Effects of pitching rotation on aerodynamics of tandem flapping

wing sections of a hovering dragonfly. E.M. Elarbi and N. Qin,

pp 699-710.

Mechanics and aerodynamics of perching manoeuvres in a large bird of prey. A.C. Carruthers, A.L.R. Thomas, S.M. Walker and G.K. Taylor, pp 673-680.

Numerical investigation of the role of hyper-mixers in supersonic mixing. S.L.N. Desikan, K. Kumaran and V. Babu, pp 659-672.

Numerical simulation of the flow field over conical, disc and flat spiked body at Mach 6. R.C. Mehta, pp

On the aerodynamics of the Miles M.52 (E.24/43) a historical perspective. B.J. Brinkworth, pp 125-156.

Supersonic aerodynamics of a projectile with slot cavities. A. Ibrahim and A. Filippone, pp 15-24.

Validation study for prediction of iced aerofoil aerodynamics. S.

Marques, K.J. Badcock, J.H.M. Gooden, S. Gates and W. Maybury, pp 103-111.

AEROELASTICITY

Non-linear system identification of the dynamics of aeroelastic instability suppression based on targeted energy transfers. Y.S. Lee, A.F. Vakakis, D.M. McFarland and L.A. Bergman, pp 61-82.

AEROSPACE ENGINEERING

6U cubeSat design for Earth observation with 6-5m GSD, five spectral bands and 14Mbps downlink. S.R. Tsitas and J. Kingston, pp 689-697.

Human-computer co-operative co-evolutionary method and its application to a satellite module layout design problem. J-Z. Huo, H-F. Teng, W. Sun and J. Chen, pp 209-223.

Linear theory of optimal hot air balloon performance application to Titan (letter). R.D. Lorentz, p 698.

Modelling ion propulsion plume interactions with spacecraft in formation flight. R. Kafafy and Y. Cao, pp 417-426.

AIRCRAFT DESIGN

An evaluation of the historical issues associated with achieving non-helicopter V/STOL capability and the search for the flying car. B. Saeed and G.B. Gratton, pp 91-102.

An innovative evaluation platform for new aircraft concepts. P. Schmollgruber, J.-L. Gobert, P.-E. Gall, Z. Goraj, H.W. Jentink, A. Nas and R. Voit-Nitchmann, pp 451-456.

Blended wing body structural concept development. A. Velicki and P. Thrash, pp 513-519.

Climate functions for the use in multi-disciplinary optimisation in the pre-design of supersonic business jet. V. Grewe, A. Stenke, M. Plohr and V.D. Korovkin, pp 259-269.

Design and realisation of a two-seater aircraft powered by fuel cell electric propulsion. G. Romeo and F. Borello, pp 281-297.

Evolution of generic flight vehicle design synthesis. B. Chudoba and W. Heinze, pp 549-567.

Hypermanoeuvrability and visual cloaking: new adaptive aerostructures technologies for UAVs. R. Barrett, pp 391-398.

NACRE novel aircraft concepts. J. Frota, pp 399-404.

THE AERONAUTICAL JOURNAL

DECEMBER 2010

BOOK REVIEWS - BY AUTHOR

Babu, V. Aircraft Propulsion, p 523.

Ben-Asher, J.Z. Optimal Control Theory with Aerospace Applications, p 522.

Chandrupatia, T.R. Quality and Reliability in Engineering, p 58.

Diston, D.J. Computational Modelling and Simulation of Aircraft and the Environment, Vol |: Platform Kinematics and Synthetic Environment, p 338.

El-Sayed, A.F. Aircraft Propulsion and Gas Turbine Engines, po2i.

Guenov, M.D. (Ed) and Kesseler, E. (Ed). Advances in Collaborative Civil Aeronautical Multidiscipinary Design Optimization, Progress in Astronautics and Aeronautics series Vol 233, p 121.

Hirschel, E.H. and Weiland, C. Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles, p 523.

Hosford, W.F. Mechanical Behavior of Materials, Second edition, p 521.

Joslin, R.D. (Ed) and Miller, D.N. (Ed). Fundamentals and applications of modern flow control, p 57.

Kang, E.W. Radar system: analysis, design and simulation, p 122.

Kesseler, E. (Ed) and Guenov, M.D. (Ed). Advances in Collaborative Civil Aeronautical Multidiscipinary Design Optimization, Progress in Astronautics and Aeronautics series Vol 233, p 121.

Miller, D.N. and Joslin, R.D. Fundamentals and Applications of Modern Flow Control, p 57.

Musoff, H. and Zarchan, P. Fundamentals of Kalman filtering: a Practical Approach, Third edition, Progress in Astronautics and Aeronautics series Vol 232, p 121.

Norstrud, H. (Ed) Sport Aerodynamics, p 610.

Obert, E. Aerodynamic Design of Transport Aircraft, p 523.

Pavlovic, P. and Pavlovic, N. Fighter Performance in Practice: Phantom versus MiG-21 How to do Split-S in MiG-21 within 3,000ft: Unexploited Low Speed Maneuverabilty, p 339 (correction on p 524).

Phillips, W.F. Mechanics of Flight, Second edition, p 338.

Przemieniecki, J.S. Finite Element Structural Analysis: New Concepts, p 122.

Raol, J.R. and Singh, J. Flight Mechanics Modeling and Analysis, p 338.

Segal, C. The Scramjet Engine: Processes and Characteristics, p 524.

Shabana, A.A. Computational Dynamics, Third edition, p 610.

Singh, J. and Raol, J.R. Flight Mechanics Modeling and Analysis, p 338.

Sridharan, S. (Ed) Delamination Behaviour of Composites, p 121.

Subcan, S. and Zbikowski, R. Computational Optimal Control: Tools and Practice, p 522.

Tennekes, H. The Simple Science of Flight: from Insects to Jumbo Jets, Revised and expanded edition, p 610.

Weiland, C. and Hirschel, E.H. Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles, p 523.

Zarchan, P. and Musoff, H. Fundamentals of Kalman Filtering: a Practical Approach, Third edition, Progress in Astronautics and Aeronautics series Vol 232, p 121.

Zbikowski, R. and Subcan, S. Computational Optimal Control: Tools and Practice, p 522.

BOOK REVIEWS - BY TITLE

Advances in Collaborative Civil Aeronautical Multidiscipinary Design Optimization. Progress in Astronautics and Aeronautics series Vol 233. E. Kesseler (Ed) and M.D. Guenov (Ed), p 121.

Aerodynamic Design of Transport Aircraft. E. Obert, p 523.

Aircraft Propulsion. V. Babu, p 523.

Aircraft Propulsion and Gas Turbine Engines. A.F. El-Sayed, p 521.

Computational Dynamics, Third edition. A.A. Shabana, p 610.

Computational Modelling and Simulation of Aircraft and the Environment Vol 1: Platform Kinematics and Synthetic Environment. D.J. Diston, p 338.

Computational Optimal Control: Tools and Practice. S. Subcan and R. Zbikowski, p 522.

Delamination Behaviour of Composites. S. Sridharan (Ed), p 121.

Fighter Performance in Practice: Phantom versus MiG-21 How to do Split-S in MiG-21 within 3,000ft: Unexploited Low Speed Maneuverabilty. P. Pavlovic and N. Pavlovic, p 339.

Finite Element Structural Analysis: New Concepts. J.S. Przemieniecki, p 122.

Flight mechanics Modeling and Analysis. J.R. Raol and J. Singh, p 338.

Fundamentals and Applications of Modern Flow Control. R.D. Joslin (Ed) and D.N. Miller (Ed), p 57.

Fundamentals of Kalman Filtering: A Practical Approach, Third edition, Progress in Astronautics and Aeronautics series Vol 232. P. Zarchan and H. Musoff, p 121.

Mechanical Behavior of Materials, Second edition. W.F. Hosford, p 521.

Mechanics of Flight, Second edition. W.F. Phillips, p 338.

Optimal Control Theory with Aerospace Applications. J.Z. Ben- Asher, p 522.

Quality and Reliability in Engineering. T.R. Chandrupatia, p 58.

Radar System: Analysis, Design and Simulation. E.W. Kang, p 122:

Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles. E.H. Hirschel and C. Weiland, p 523.

Sport Aerodynamics. H. Norstrud (Ed), p 610.

The Scramjet Engine: Processes and Characteristics. C. Segal, p 524.

The Simple Science of Flight: From Insects to Jumbo Jets, Revised and expanded edition. H. Tennekes, p 610.

COMPOSITES Nonlinear transient analysis of moderately thick rectangular composite plates. H. Tanréver and E. Senocak, pp 437-444.

COMPUTATIONAL FLUID DYNAMICS

Helicopter icing. Y. Cao and K. Chen, pp 83-90.

Numerical simulation of the flow field over conical, disc and flat spiked body at Mach 6. R.C. Mehta, pp 225-236.

COMPUTATIONAL TECHNIQUES

Analysis of turbine performance degradation effects due to geometry variations between actual components and design intent. P.K. Zachos and A.I. Kalfas, pp 569-578.

Application of a knowledge based design methodology to support fuselage panel design. S.W.G van der Elst, M.J.L. van Tooren, B. Vermeulen, C.L. Emberey and N.R. Milton, pp 589-597.

Development and validation of an efficient direct numerical optimization approach for aerofoil shape design. M. Khurana and H. Winarto, pp 611-628.

INDEX TO VOLI

ME 114 787

Load transportation system based on autonomous small size helicopters. M. Bernard, K. Kondak and G. Hommel, pp 191-198.

Nonlinear transient analysis of moderately thick rectangular composite plates. H. Tanréver and E. ?enocak, pp 437-444.

Recent extensions and applications of the ‘CST’ universal parametric geometry representation method. B.M. Kulfan, pp 157-176.

Starting characteristics of a rectangular supersonic air-intake

with cowl deflection. S. Das and J.K. Prasad, pp 177-189.

ENVIRONMENTAL ENGINEERING

Aviation and climate change: confronting the challenge. A. Bows, pp 459-468.

Climate functions for the use in multi-disciplinary optimisation in the pre-design of supersonic business jet. V. Grewe, A. Stenke, M. Plohr and V.D. Korovkin, pp 259-269.

Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project. V. Grewe, M. Plohr, G. Cerino, M. Di Muzio, Y. Deremaux, M. Galerneau, P. de Saint Martin, T. Chaika, A. Hasselrot, U. Tengzelius and V.D. Korovkin, pp 199-206.

FLIGHT CONTROL

An overview of experiments on the dynamic sensitivity of MAVs to turbulence. S. Watkins, M. Abdulrahim, M. Thompson, M. Shortis, R. Segal and J. Sheridan, pp 485-492.

Maximum entropy approach to the identification of stochastic reduced-order models of nonlinear dynamical systems. M. Arnst, R. Ghanem and S. Masri, pp 637-650.

New methodology and code for Hawker 800XP aircraft stability derivatives calculation from geometrical data. N. Anton, R.M. Botez and D. Popescu, pp 367-376.

Performing co-ordinated turns with articulated wing-tips as multi-axis control effectors. P. Bourdin,, A. Gatto and M.I. Friswell, pp 35-47.

Upset recovery training, lessons from accidents and incidents. D.A. Crider, pp 629-636.

Investigation of Chinock helicopter operations with an external slung load after cable failure. M.D. Pavel, pp 345-365.

FLIGHT CONTROL SYSTEMS

Flight control using pin-protuberances for blunted cones. R. Samar, S. Zahir and M.A. Khan, pp 245-257.

Flutter control using resistively shunted piezoceramics. S.B. Kandagal and K. Venkatraman, pp 387-390.

Investigation of rotorcraft-pilot couplings under flight-path constraint below the minimum-power speed. L. Lu, G.D. Padfield and M. Jump, pp 405-416.

New adaptive controller method for SMA hysteresis modeling of

a morphing wing. T.L. Grigorie and R.M. Botez, pp 1-13.

FLIGHT SIMULATION The impact of flight simulation in aerospace. D.J. Allerton, pp 747-756.

HISTORY On the aerodynamics of the Miles M.52 (E.24/43) a historical perspective. B.J. Brinkworth, pp 125-156.

LIGHTER THAN AIR Linear theory of optimal hot air balloon performance application to Titan (letter). R.D. Lorentz, p 698.

MANUFACTURING

Design support for metallic machined ribs using knowledge based engineering techniques. T. van der Laan, F. van Dalen and B. Vermeulen, pp 681-688.

PROPULSION

Supersonic aerodynamics of a projectile with slot cavities. A Ibrahim and A. Filippone, pp 15-24.

Analysis of turbine performance degradation effects due to geometry variations between actual components and design Intent. P.K. Zachos and A.I. Kalfas, pp 569-578.

Design and realisation of a two-seater aircraft powered by fuel cell electric propulsion. G. Romeo and F. Borello, pp 281-297.

Enhanced vortex stability in trapped vortex combustor, Technical Note. S. Vengadesan and C. Sony, pp 333-337.

Modelling ion propulsion plume interactions with spacecraft in formation flight. R. Kafafy and Y. Cao, pp 417-426.

Numerical investigation of the role of hyper-mixers in supersonic mixing. S.L.N. Desikan, K. Kumaran and V. Babu, pp 659-672.

Starting characteristics of a rectangular supersonic air-intake with cowl deflection. S. Das and J.K. Prasad, pp 177-189.

ROTORCRAFT

Helicopter icing. Y. Cao and K. Chen, pp 83-90.

Investigation of Chinook helicopter operations with an external slung load after cable failure. M.D. Pavel, pp 345-365.

Investigation of rotorcraft-pilot couplings under flight-path constraint below the minimum-power speed. L. Lu, G.D. Padfield and M. Jump, pp 405-416.

Load transportation system based on autonomous small size helicopters. M. Bernard, K. Kondak and G. Hommel, pp 191-198.

Simulation of automatic helicopter deck landings using nature inspired flight control. M. Voskuijl, G.D. Padfield, D.J. Walker, B.J. Manimala and A.W. Gubbels, pp 25-34.

SAFETY

Adaptive moving average for trending of accident rates, Technical Note. M. Merens, pp 711-713.

Computer model for numerical simulation of emergency evacuation of transport airplanes. J.M. Hedo and R. Martinez- Val, pp 737-746.

Fire and evacuation analysis in BWB aircraft configurations: computer simulations and large-scale evacuation experiment. E.R. Galea, L. Filippidis, Z. Wang and J. Ewer, pp 271-277.

Implicit large eddy simulation of ship airwakes. B. Thornber, M. Starr and D. Drikakis, pp 715-736.

Upset recovery training lessons from accidents and incidents. D.A. Crider, pp 629-636.

SIMULATION

Computer model for numerical simulation of emergency evacuation of transport airplanes. J.M. Hedo and R. Martinez- Val, pp 737-746.

Simulation of automatic helicopter deck landings using nature inspired flight control. M. Voskuijl, G.D. Padfield, D.J. Walker, B.J. Manimala and A.W. Gubbels, pp 25-34.

STRUCTURES

A comprehensive numerical study of battle damage and repairs upon the aerodynamic characteristics of an aerofoil. M. Saeedi,

F, Ajalli and M. Mani, pp 469-484.

THE AERONAUTICAL JOURNAL

DECEMBER 2010

A finite element stress analysis of aircraft bolted joints loaded in tension. R.H. Oskouei, M. Keikhosravy and C. Soutis, pp 315- 320.

Application of a knowledge based design methodology to support fuselage panel design. S.W.G van der Elst, M.J.L. van Tooren, B. Vermeulen, C.L. Emberey and N.R. Milton, pp 589-597.

Aspects of battle damage repair of helicopter structures. J. Wang and A. Baker, pp 321-332.

Blended wing body structural concept development. A. Velicki and P. Thrash, pp 513-519.

Design support for metallic machined ribs using knowledge based engineering techniques. T. van der Laan, F. van Dalen and B. Vermeulen, pp 681-688.

Exact strip analysis and optimum design of aerospace structures. D. Kennedy and C.A. Featherston, pp 505-512.

Goodness dispersion curves for ultrasonic guided wave based SHM: a sample problem in corrosion monitoring. H. Gao and J.L. Rose, pp 49-56.

SYSTEMS

6U cubeSat design for Earth observation with 6-5m GSD, five spectral bands and 14Mbps downlink. S.R. Tsitas and J. Kingston, pp 689-697.

Improved test capabilities for cost-effective performance evaluation of airborne electronic warfare systems. M. Pywell and M. Midgley-Davies, pp 527-547.

New adaptive controller method for SMA hysteresis modeling of a morphing wing. T.L. Grigorie and R.M. Botez, pp | to 13. Operation of small sensor payloads on tactical sized unmanned

air vehicles. M.C.L. Patterson and A. Brescia, pp 427-436.

Radar target tracking in cluttered environment based on particle

filtering. N. Huansheng, C. Weishi and L. Jing, pp 309-314.

TESTING FACILITIES

Improved test capabilities for cost-effective performance evaluation of airborne electronic warfare systems. M. Pywell and M. Midgley-Davies, pp 527-547.

UNMANNED AERIAL VEHICLES

An overview of experiments on the dynamic sensitivity of MAVs to turbulence. S. Watkins, M. Abdulrahim, M. Thompson, M. Shortis, R. Segal and J. Sheridan, pp 485-492.

Hypermanoeuvrability and visual cloaking: new adaptive aerostructures technologies for UAVs. R. Barrett, pp 391-398.

Operation of small sensor payloads on tactical sized unmanned air vehicles. M.C.L. Patterson and A. Brescia, pp 427-436.

UNSTEADY AERODYNAMICS

Computational and experimental study of intake ground vortices. S. Zantopp, D. MacManus and J. Murphy, pp 769-784.

Effects of boundary layer bleeding on unstart oscillatory flow of hypersonic inlets. J. Chang, W. Bao and D. Yu, pp 445-450.

Enhanced vortex stability in trapped vortex combustor, Technical Note. S. Vengadesan and C. Sony, pp 333-337.

Experimental study of unsteadiness in supersonic shock- wave/turbulent boundary-layer interactions with separation. D. Estruch, D.G. MacManus,, D.P. Richardson, N.J. Lawson, K.P. Garry and J.L. Stollery, pp 299-308.

Measurements of velocity field in the wake of an oscillating wind turbine blade. M.R. Soltani and M. Mahmoudi, pp 493-504.

Wake vortex encounters in a flight simulator. D.J. Allerton and G.T. Spence, pp 579-587.

WAKES Wake vortex encounters in a flight simulator. D.J. Allerton and G.T. Spence, pp 579-587.

DECEMBER 2010

INDEX TO VOLUME 114

Author Index

ABDULRAHIM, M., THOMPSON, M., SHORTIS, M., SEGAL, R., SHERIDAN, J. and WATKINS, S. An overview of experiments on the dynamic sensitivity of MAVs to turbulence, pp 485-492.

AJALLI, F., MANI, M. and SAEEDI, M. A comprehensive numerical study of battle damage and repairs upon the aerodynamic characteristics of an aerofoil, pp 469-484.

ALLERTON, D.J. and SPENCE, G.T. Wake vortex encounters in a flight simulator, pp 579-587.

ALLERTON, D.J.

The impact of flight simulation in aerospace, pp 747-756.

ANTON, N., BOTEZ, R.M. and POPESCU, D. New methodology and code for Hawker 800XP aircraft stability derivatives calculation from geometrical data, pp 367-376.

ARNST, M., GHANEM, R. and MASRI, S. Maximum entropy approach to the identification of stochastic reduced- order models of nonlinear dynamical systems, pp 637-650.

BABU, V., DESIKAN, S.L.N. and KUMARAN, K. Numerical investigation of the role of hyper-mixers in supersonic mixing, pp 659-672.

BADCOCK, K.J., GOODEN, J.H.M., GATES, S., MAYBURY, W. and MARQUES, S. Validation study for prediction of iced aerofoil aerodynamics, pp 103- ERE

BAKER, A. and WANG, J.

BAO, W., YU, D. and CHANG, J. Effects of boundary layer bleeding on unstart oscillatory flow of hypersonic inlets, pp 445-450.

BARRETT, R. Hypermanoeuvrability and visual cloaking: new adaptive aerostructures technologies for UAVs, pp 391-398.

BERGMAN, L.A., LEE, Y.S., VAKAKIS, A.F. and MCFARLAND, D.M. Non-linear system identification of the dynamics of aeroelastic instability suppression based on targeted energy transfers, pp 61-82.

BERNARD, M., KONDAK, K. and HOMMEL, G. Load transportation system based on autonomous small size helicopters, pp 191-198.

BOND, I.P., JONES, D.P., THILL, C., DOWNSBOROUGH, J.D. AND LAI, S.J. Aerodynamic study of corrugated skins for morphing wing applications, pp 237-244.

BORELLO, F. and ROMEO, G. Design and realisation of a two-seater aircraft powered by fuel cell electric propulsion, pp 281-297.

BOTEZ, R.M. and GRIGORIE, T.L. New adaptive controller method for SMA hysteresis modeling of a morphing wing, pp | -13.

BOTEZ, R.M., POPESCU, D. and ANTON, N. New methodology and code for Hawker 800XP aircraft stability derivatives calculation from geometrical data, pp 367-376.

BOURDIN, P., GATTO, A. and FRISWELL, M.I. Performing co-ordinated turns with articulated wing-tips as multi-axis control effectors, pp 35-47.

BOWS, A. Aviation and climate change: confronting the challenge, pp 459-468.

BRESCIA, A. and PATTERSON, M.C.L. Operation of small sensor payloads on tactical sized unmanned air vehicles, pp 427-436.

BRINKWORTH, B.J. On the aerodynamics of the Miles M.52 (E.24/43) a historical perspective, pp 125-156.

CAIN, T. The effect of gravity on a shaped sonic boom, pp 651-656.

CAO, Y. and CHEN, K. Helicopter icing, pp 83-90.

CAO, Y. and KAFAFY, R. Modelling ion propulsion plume interactions with spacecraft in formation flight, pp 417-426.

CARRUTHERS, A.C., THOMAS, A.L.R., WALKER, S.M. and TAYLOR, G.K. Mechanics and aerodynamics of perching manoeuvres in a large bird of prey, pp 673-680.

CERINO, G., DI MUZIO, M., DEREMAUX, Y., GALERNEAU, M., DE SAINT MARTIN, P., CHAIKA, T., HASSELROT, A., TENGZELIUS, U., KOROVKIN, V.D., GREWE, V. and PLOHR M. Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

CHAIKA, T., HASSELROT, A., TENGZELIUS, U., KOROVKIN, V.D., GREWE, V., PLOHR, M., CERINO, G., DI MUZIO, M.., DEREMAUX, Y., GALERNEAU, M. and DE SAINT MARTIN, P. Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

CHANG, J., BAO, W. and YU, D. Effects of boundary layer bleeding on unstart oscillatory flow of hypersonic inlets, pp 445-450.

CHEN, K. and CAO, Y. Helicopter icing, pp 83-90.

CHEN, J., HUO, J-Z., TENG, H-F. and SUN, W. Human-computer co-operative co-evolutionary method and its application to a satellite module layout design problem, pp 209-223.

CHUDOBA, B. and HEINZE, W. Evolution of generic flight vehicle design synthesis, pp 549-567.

CINIGLIO, U., CORRARO, F., VITALE, A., GENITO, N. and GARBARINO, L. A hybrid frequency-time domain technique for ground effect identification, pp 377-385.

THE AERONAUTICAL JOURNAI DECEMBER 2010

CORRARO, F., VITALE, A., GENITO, N., GARBARINO, L. and CINIGLIO, U. A hybrid frequency-time domain technique for ground effect identification, pp 377-385.

CRIDER, D.A. Upset recovery training, lessons from accidents and incidents, pp 629-636.

D°’HUMIERES, G. and STOLLERY, J.L. Drag reduction on a spiked body at hypersonic speed, pp 113-119.

DAS, S. and PRASAD, J.K. Starting characteristics of a rectangular supersonic air-intake with cowl deflection, pp 177-189.

DE SAINT MARTIN, P., CHAIKA, T., HASSELROT, A., TENGZELIUS, U., KOROVKIN, V.D., GREWE, V., PLOHR, M., CERINO, G., DI MUZIO, M., DEREMAUX, Y. and GALERNEAU, M.

Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

DEREMAUX, Y., GALERNEAU, M., DE SAINT MARTIN, P., CHAIKA, T., HASSELROT, A., TENGZELIUS, U., KOROVKIN, V.D., GREWE, V., PLOHR, M., CERINO, G. and DI MUZIO, M. Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

DESIKAN, S.L.N., KUMARAN, K. and BABU, V. Numerical investigation of the role of hyper-mixers in supersonic mixing, pp 659-672.

DI MUZIO, M., DEREMAUX, Y., GALERNEAU, M., DE SAINT MARTIN, P., CHAIKA, T., HASSELROT, A., TENGZELIUS, U., KOROVKIN, V.D., GREWE, V., PLOHR, M. and CERINO, G. Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

DOWNSBOROUGH, J.D., LAI, S.J., BOND, I.P., JONES, D.P. and THILL, C.

Aerodynamic study of corrugated skins for morphing wing applications, pp 237-244.

DRIKAKIS, D., THORNBER, B. and STARR, M. Implicit large eddy simulation of ship airwakes, pp 715-736.

ELARBI, E.M. and QIN, N.

Effects of pitching rotation on aerodynamics of tandem flapping wing sections of a hovering dragonfly, pp 699-710.

EMBEREY, C.L., MILTON, N.R., VAN DER ELST, S.W.G, VAN TOOREN, M.J.L. and VERMEULEN, B. Application of a knowledge based design methodology to support fuselage panel design, pp 589-597.

ESTRUCH, D., MACMANUS, D.G., RICHARDSON, D.P., LAWSON, N.J., GARRY, K.P. and STOLLERY, J.L. Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation, pp 299-308.

EWER, J., GALEA, E.R., FILIPPIDIS, L. and WANG, Z. Fire and evacuation analysis in BWB aircraft configurations: computer simulations and large-scale evacuation experiment, pp 271-277.

FEATHERSTON, C.A. and KENNEDY, D.

Exact strip analysis and optimum design of aerospace structures, pp 505-512.

FILIPPIDIS, L., WANG, Z., EWER, J. and GALEA, E.R. Fire and evacuation analysis in BWB aircraft configurations: computer simulations and large-scale evacuation experiment, pp 271-277.

FILIPPONE, A. and IBRAHIM, A. Supersonic aerodynamics of a projectile with slot cavities, pp 15-24.

FRISWELL, M.I., BOURDIN, P. and GATTO, A. Performing co-ordinated turns with articulated wing-tips as multi-axis control effectors, pp 35-47.

FROTA, J. NACRE novel aircraft concepts, pp 399-404.

GALEA, E.R., FILIPPIDIS, L., WANG, Z. and EWER, J. Fire and evacuation analysis in BWB aircraft configurations: computer simulations and large-scale evacuation experiment, pp 271-277.

GALERNEAU, M., DE SAINT MARTIN, P., CHAIKA, T., HASSELROT, A., TENGZELIUS, U., KOROVKIN, V.D., GREWE, V., PLOHR, M., CERINO, G., DI MUZIO, M. and DEREMAUX, Y.

Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

GALL, P.-E., GORAJ, Z., JENTINK, H.W., NAS, A., VOIT- NITCHMANN, R., SCHMOLLGRUBER, P. and GOBERT, J.-L. An innovative evaluation platform for new aircraft concepts, pp 451-456.

GAO, H. and ROSE, J.L. Goodness dispersion curves for ultrasonic guided wave based SHM: a sample problem in corrosion monitoring, pp 49-56.

GARBARINO, L., CINIGLIO, U., CORRARO, F., VITALE, A. and GENITO, N. A hybrid frequency-time domain technique for ground effect identification, pp 377-385.

GARRY, K.P., STOLLERY, J.L., ESTRUCH, D., MACMANUS, D.G., RICHARDSON, D.P. and LAWSON, N.J. Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation, pp 299-308.

GATES, S., MAYBURY, W., MARQUES, S., BADCOCK, K.J. and GOODEN, J.H.M. Validation study for prediction of iced aerofoil aerodynamics, pp 103- 111.

GATTO, A., FRISWELL, M.I. and BOURDIN, P. Performing co-ordinated turns with articulated wing-tips as multi-axis control effectors, pp 35-47.

GENITO, N., GARBARINO, L., CINIGLIO, U., CORRARO, F. and VITALE, A. A hybrid frequency-time domain technique for ground effect identification, pp 377-385.

GHANEM, R., MASRI, S. and ARNST, M. Maximum entropy approach to the identification of stochastic reduced- order models of nonlinear dynamical systems, pp 637-650.

GOBERT, J.-L., GALL, P.-E., GORAJ, Z., JENTINK, H.W., NAS, A.., VOIT-NITCHMANN, R. and SCHMOLLGRUBER, P. An innovative evaluation platform for new aircraft concepts, pp 451- 456.

GOODEN, J.H.M., GATES, S., MAYBURY, W., MARQUES, S. and BADCOCK, K.J. Validation study for prediction of iced aerofoil aerodynamics, pp 103- Pet.

GORAJ, Z., JENTINK, H.W., NAS, A., VOIT-NITCHMANN, R., SCHMOLLGRUBER, P., GOBERT, J.-L. and GALL, P.-E. An innovative evaluation platform for new aircraft concepts, pp 451-456.

INDEX TO VOLUME 114 79]

GRATTON, G.B. and SAEED, B. An evaluation of the historical issues associated with achieving non- helicopter V/STOL capability and the search for the flying car, pp 91- 102.

GREWE, V., STENKE, A., PLOHR, M. and KOROVKIN, V.D. Climate functions for the use in multi-disciplinary optimisation in the pre-design of supersonic business jet, pp 259-269.

GREWE, V., PLOHR, M., CERINO, G., DI MUZIO, M., DEREMAUX, Y., GALERNEAU, M., DE SAINT MARTIN, P., CHAIKA, T., HASSELROT, A., TENGZELIUS, U. and KOROVKIN, V.D.

Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project , pp199-206.

GRIGORIE, T.L. and BOTEZ, R.M. New adaptive controller method for SMA hysteresis modeling of a morphing wing, pp I-13

GUBBELS, A.W., VOSKULJL, M., PADFIELD, G.D., WALKER, D.J. and MANIMALA, B.J. Simulation of automatic helicopter deck landings using nature inspired flight control, pp 25-34

HARTJES, S., VISSER, H.G. and HEBLY, S.J Optimisation of RNAV noise and emission abatement standard instrument departures, pp 757-767

HASSELROT, A., TENGZELIUS, U., KOROVKIN, V.D., GREWE, V., PLOHR, M., CERINO, G., DI MUZIO, M., DEREMAUX, Y., GALERNEAU, M., DE SAINT MARTIN, P. and CHAIKA T. Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

HEBLY, S.J., HARTJES, S. and VISSER, H.G. Optimisation of RNAV noise and emission abatement standard instrument departures, pp 757-767

HEDO, J.M. and MARTINEZ-VAL, R.

Computer model for numerical simulation of emergency evacuation of transport airplanes, pp 737-746

HEINZE, W. and CHUDOBA, B.

Evolution of generic flight vehicle design synthesis, pp 549-567.

HOMMEL, G., BERNARD, M. and KONDAK, K. Load transportation system based on autonomous small size helicopters,

pp 191-198.

HUANSHENG, N., WEISHI, C. and JING, L. Radar target tracking in cluttered environment based on particle filtering,

pp 309-314.

HUO, J-Z., TENG, H-F., SUN, W. and CHEN, J. Human-computer co-operative co-evolutionary method and its application to a satellite module layout design problem, pp 209-223.

IBRAHIM, A. and FILIPPONE, A. Supersonic aerodynamics of a projectile with slot cavities, pp 15-24.

JENTINK, H.W., NAS, A., VOIT-NITCHMANN, R., SCHMOLLGRUBER, P., GOBERT, J.-L., GALL P.-E. and GORAJ, Z.

An innovative evaluation platform for new aircraft concepts, pp 451- 456.

JING, L., HUANSHENG, N. and WEISHI, C. Radar target tracking in cluttered environment based on particle filtering, pp 309-314.

JONES, D.P., THILL, C., DOWNSBOROUGH, J.D., LAI, S.J. and BOND, LP.

Aerodynamic study of corrugated skins for morphing wing applications, pp 237-244.

JUMP, M., LU, L. and PADFIELD, G.D. Investigation of rotorcraft-pilot couplings under flight-path constraint below the minimum-power speed, pp 405-416.

KAFAFY, R. and CAO, Y. Modelling ion propulsion plume interactions with spacecraft in formation flight, pp 417-426.

KALFAS, A.I. and ZACHOS, P.K. Analysis of turbine performance degradation effects due to geometry variations between actual components and design intent, pp 569-578

KANDAGAL, S.B. and VENKATRAMAN, K.

Flutter control using resistively shunted piezoceramics, pp 387-390.

KEIKHOSRAVY, M., SOUTIS, C. and OSKOUEI, R.H.

\ finite element stress analysis of aircraft bolted joints loaded in tension,

pp 315-320

KENNEDY, D. and FEATHERSTON, C.A.

Exact strip analysis and optimum design of aerospace structures, pp 505-

512

KHAN, M.A., SAMAR, R. and ZAHIR, S. Flight control using pin-protuberances for blunted cones, pp 245-25

KHURANA, M. and WINARTO, H. Development and validation of an efficient direct numerical optimization approach for aerofoil shape design, pp 611-628

KINGSTON, J. and TSITAS, S.R. 6U cubeSat design for Earth observation with 6-5m GSD, five spectral bands and 14Mbps downlink, pp 689-697.

KONDAK, K., HOMMEL, G. and BERNARD, M. Load transportation system based on autonomous small size helicopters, pp 191-198.

KOROVKIN, V.D., GREWE, V., STENKE, A. and PLOHR, M. Climate functions for the use in multi-disciplinary optimisation in the

pre-design of supersonic business jet, pp 259-269.

KOROVKIN, V.D., GREWE, V., PLOHR, M., CERINO, G., DI MUZIO, M., DEREMAUX, Y., GALERNEAU, M., DE SAINT MARTIN, P., CHAIKA, T., HASSELROT, A. and TENGZELIUS, U. Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

KULFAN, B.M. Recent extensions and applications of the CST universal parametric geometry representation method, pp 157-176.

KUMARAN, K., BABU, V. and DESIKAN, S.L.N. Numerical investigation of the role of hyper-mixers in supersonic mixing, pp 659-672.

LAI, S.J., BOND, I.P., JONES, D.P., THILL, C. and DOWNSBOROUGH, J.D. Aerodynamic study of corrugated skins for morphing wing applications, pp 237-244.

LAWSON, N.J., GARRY, K.P., STOLLERY, J.L., ESTRUCH, D., MACMANUS, D.G. and RICHARDSON, D.P. Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation, pp 299-308.

792

THE AERONAU’

TICAL JOURNAL DECEMBER 2010

LEE, Y.S., VAKAKIS, A.F., MCFARLAND, D.M. and BERGMAN, L.A. Non-linear system identification of the dynamics of aeroelastic instability suppression based on targeted energy transfers, pp 61-82.

LORENTZ, R.D. Letter Linear theory of optimal hot air balloon performance application to Titan, pp 698.

LU, L., PADFIELD, G.D. and JUMP, M. Investigation of rotorcraft-pilot couplings under flight-path constraint below the minimum-power speed, pp 405-416.

MACMANUS, D., MURPHY, J. and ZANTOPP, S. Computational and experimental study of intake ground vortices, pp 769-784.

MACMANUS, D.G., RICHARDSON, D.P., LAWSON, N.J., GARRY, K.P., STOLLERY, J.L. and ESTRUCH, D. Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation, pp 299-308.

MAHMOUDIL, M. and SOLTANI, MLR. Measurements of velocity field in the wake of an oscillating wind turbine blade, pp 493-504.

MANI, M., SAEEDI, M. and AJALLI, F. A comprehensive numerical study of battle damage and repairs upon the aerodynamic characteristics of an aerofoil, pp 469-484.

MANIMALA, B.J., GUBBELS, A.W., VOSKUIJL, M., PADFIELD, G.D. and WALKER, D.J. Simulation of automatic helicopter deck landings using nature inspired flight control, pp 25-34.

MARQUES, S., BADCOCK, K.J., GOODEN, J.H.M., GATES, S. and MAYBURY, W. Validation study for prediction of iced aerofoil aerodynamics, pp 103-111.

MARTINEZ-VAL, R. and HEDO, J.M. Computer model for numerical simulation of emergency evacuation of transport airplanes, pp 737-746.

MASRI, S., ARNST, M. and GHANEM, R. Maximum entropy approach to the identification of stochastic reduced- order models of nonlinear dynamical systems, pp 637-650.

MAYBURY, W., MARQUES, S., BADCOCK, K.J., GOODEN, J.H.M. and GATES, S.

Validation study for prediction of iced aerofoil aerodynamics, pp 103-111.

MCFARLAND, D.M., BERGMAN, L.A., LEE, Y.S. and VAKAKIS, A.F. Non-linear system identification of the dynamics of aeroelastic instability suppression based on targeted energy transfers, pp 61-82.

MEHTA, R.C.

Numerical simulation of the flow field over conical, disc and flat spiked body at Mach 6, pp 225-236.

MERENS, M.

Adaptive moving average for trending of accident rates, Technical Note, pp 711-713.

MIDGLEY-DAVIES, M. and PYWELL, M. Improved test capabilities for cost-effective performance evaluation of airborne electronic warfare systems, pp 527-547.

MILTON, N.R., VAN DER ELST, S.W.G, VAN TOOREN, M.J.L., VERMEULEN, B. and EMBEREY, C.L. Application of a knowledge based design methodology to support fuselage panel design, pp 589-597.

MURPHY, J., ZANTOPP, S. and MACMANUS, D. Computational and experimental study of intake ground vortices, pp 769-784.

NAS, A., VOIT-NITCHMANN, R., SCHMOLLGRUBER, P., GOBERT, J.-L., GALL, P.-E., GORAJ, Z. and JENTINK, H.W. An innovative evaluation platform for new aircraft concepts, pp 451- 456.

OSKOUEI, R.H., KEIKHOSRAVY, M. and SOUTIS, C. A finite element stress analysis of aircraft bolted joints loaded in tension, pp 315-320.

PADFIELD, G.D., JUMP, M. and LU, L. Investigation of rotorcraft-pilot couplings under flight-path constraint below the minimum-power speed, pp 405-416.

PADFIELD, G.D., WALKER, D.J., MANIMALA, B.J., GUBBELS, A.W. and VOSKUIJL, M. Simulation of automatic helicopter deck landings using nature inspired flight control, pp 25-34.

PATTERSON, M.C.L. and BRESCIA, A. Operation of small sensor payloads on tactical sized unmanned air vehicles, pp 427-436.

PAVEL, M.D. Investigation of Chinook helicopter operations with an external slung load after cable failure, pp 345-365.

PLOHR, M., CERINO, G., DI MUZIO, M., DEREMAUX, Y., GALERNEAU, M., DE SAINT MARTIN, P., CHAIKA, T., HASSELROT, A., TENGZELIUS, U., KOROVKIN, V.D. and GREWE, V.

Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

PLOHR, M., KOROVKIN, V.D., GREWE, V. and STENKE, A. Climate functions for the use in multi-disciplinary optimisation in the pre-design of supersonic business jet, pp 259-269.

POPESCU, D., ANTON, N. and BOTEZ, R.M. New methodology and code for Hawker 800XP aircraft stability derivatives calculation from geometrical data, pp 367-376.

PRASAD, J.K. and DAS, S. Starting characteristics of a rectangular supersonic air-intake with cowl deflection, pp 177-189.

PYWELL, M. and MIDGLEY-DAVIES, M. Improved test capabilities for cost-effective performance evaluation of airborne electronic warfare systems, pp 527-547.

QIN, N. and ELARBI, E.M. Effects of pitching rotation on aerodynamics of tandem flapping wing sections of a hovering dragonfly, pp 699-710.

RICHARDSON, D.P., LAWSON, N.J., GARRY, K.P., STOLLERY, J.L., ESTRUCH, D. and MACMANUS, D.G. Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation, pp 299-308.

ROMEO, G. and BORELLO, F. Design and realisation of a two-seater aircraft powered by fuel cell electric propulsion, pp 281-297.

ROSE, J.L. and GAO, H. Goodness dispersion curves for ultrasonic guided wave based SHM: a sample problem in corrosion monitoring, pp 49-56.

INDEX TO VOLUME 114

ROSSOW, C.-C. Aerodynamics A discipline swept away?, pp 599-609.

SAEED, B. and GRATTON, G.B. An evaluation of the historical issues associated with achieving non- helicopter V/STOL capability and the search for the flying car 91-102.

SAEEDI, M., AJALLI, F. and MANI, M. A comprehensive numerical study of battle damage and repairs upon the aerodynamic characteristics of an aerofoil 469-484.

SAMAR, R., ZAHIR, S. and KHAN, M.A. Flight control using pin-protuberances for blunted cone

SCHMOLLGRUBER, P., GOBERT, J.-L., GALL, P.-E., GORAJ, Z.., JENTINK, H.W., NAS, A. and VOIT-NITCHMANN, R. An innovative evaluation platform for new aircraft concepts, pp 451-456.

SEGAL, R., SHERIDAN, J., WATKINS, S., ABDULRAHIM, M., THOMPSON, M. and SHORTIS, M. An overview of experiments on the dynamic sensitivity of MAVs to turbulence, pp 485-492.

SENOCAK, E. and TANROVER, H. Nonlinear transient analysis of moderately thick rectangular composite plates, pp 437-444.

SHERIDAN, J., WATKINS, S., ABDULRAHIM, M., THOMPSON, M., SHORTIS, M. and SEGAL, R. An overview of experiments on the dynamic sensitivity of MAVs to turbulence, pp 485-492.

SHORTIS, M., SEGAL, R., SHERIDAN, J., WATKINS, S., ABDULRAHIM, M. and THOMPSON, M. An overview of experiments on the dynamic sensitivity of MAVs to turbulence, pp 485-492.

SOLTANI, M.R. and MAHMOUDI, M. Measurements of velocity field in the wake of an oscillating wind turbine blade, pp 493-504.

SONY, C. and VENGADESAN, S. Enhanced vortex stability in trapped vortex combustor, Technical Note, pp 333-337.

SOUTIS, C., OSKOUEI, R.H. and KEIKHOSRAVY, M. A finite element stress analysis of aircraft bolted joints loaded in tension, pp 315-320.

SPENCE, G.T. and ALLERTON, D.J. Wake vortex encounters in a flight simulator, pp 579-587.

STARR, M., DRIKAKIS, D. and THORNBER, B. Implicit large eddy simulation of ship airwakes, pp 715-736.

STENKE, A., PLOHR, M., KOROVKIN, V.D. and GREWE, V. Climate functions for the use in multi-disciplinary optimisation in the pre-design of supersonic business jet, pp 259-269.

STOLLERY, J.L. and DPHUMIERES, G. Drag reduction on a spiked body at hypersonic speed, pp 113-119.

STOLLERY, J.L., ESTRUCH, D., MACMANUS, D.G., RICHARDSON, D.P., LAWSON, N.J. and GARRY, K.P. Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation, pp 299-308.

SUN, W., CHEN, J., HUO, J-Z. and TENG, H-F. Human-computer co-operative co-evolutionary method and its application to a satellite module layout design problem, pp 209-223.

TANROVER, H. and SENOCAK, E. Nonlinear transient analysis of moderately thick rectangular composite plates, pp 437-444.

TAYLOR, G.K., CARRUTHERS, A.C., THOMAS, A.L.R. and WALKER, S.M. Mechanics and aerodynamics of perching manoeuvres in a large bird of prey, pp 673-680.

TENG, H-F., SUN, W., CHEN, J. and HUO, J-Z. Human-computer co-operative co-evolutionary method and its application to a satellite module layout design problem, pp 209-223.

TENGZELIUS, U., KOROVKIN, V.D., GREWE, V., PLOHR, M., CERINO, G., DI MUZIO, M., DEREMAUX, Y., GALERNEAU, M., DE SAINT MARTIN, P., CHAIKA, T. and HASSELROT, A.

Estimates of the climate impact of future small-scale supersonic transport aircraft results from the HISAC EU-project, pp 199-206.

THILL, C., DOWNSBOROUGH, J.D., LAI, S.J., BOND, LP. and JONES, D.P.

Aerodynamic study of corrugated skins for morphing wing applications, pp 237-244.

THOMAS, A.L.R., WALKER, S.M., TAYLOR, G.K. and CARRUTHERS A.C. Mechanics and aerodynamics of perching manoeuvres in a large bird of prey, pp 673-680.

THOMPSON, M., SHORTIS, M., SEGAL, R., SHERIDAN, J., WATKINS, S. and ABDULRAHIM M. An overview of experiments on the dynamic sensitivity of MAVs to turbulence, pp 485-492.

THORNBER, B., STARR, M. and DRIKAKIS, D. Implicit large eddy simulation of ship airwakes, pp 715-736.

THRASH, P. and VELICKI, A. Blended wing body structural concept development, pp 513-519.

TSITAS, S.R. and KINGSTON, J. 6U cubeSat design for Earth observation with 6-S5m GSD, five spectral bands and 14Mbps downlink, pp 689-697.

"AKAKIS, A.F., MCFARLAND, D.M., BERGMAN, L.A. and LEE, Y.S. Non-linear system identification of the dynamics of aeroelastic instability suppression based on targeted energy transfers, pp 61-82.

“AN DALEN, F., VERMEULEN, B. and VAN DER LAAN, T. Design support for metallic machined ribs using knowledge based engineering techniques, pp 681-688.

‘AN DER ELST, S.W.G, VAN TOOREN, M.J.L., VERMEULEN, B., EMBEREY, C.L. and MILTON, N.R. Application of a knowledge based design methodology to support fuselage panel design, pp 589-597.

‘AN DER LAAN, T., VAN DALEN, F. and VERMEULEN, B. Design support for metallic machined ribs using knowledge based engineering techniques, pp 681-688.

VAN TOOREN, M.J.L., VERMEULEN, B., EMBEREY, C.L., MILTON, N.R. and VAN DER ELST, S.W.G. Application of a knowledge based design methodology to support fuselage panel design, pp 589-597.

VELICKI, A. and THRASH, P. Blended wing body structural concept development, pp 513-519.

794 THE AERONAUTICAL JOURNAL

DECEMBER 2010

VENGADESAN, S. and SONY, C. Enhanced vortex stability in trapped vortex combustor, Technical Note,

VENKATRAMAN, K. and KANDAGAL, S.B. Flutter control using resistively shunted piezoceramics, pp 387-390.

VERMEULEN, B., VAN DER LAAN, T. and VAN DALEN, F. Design support for metallic machined ribs using knowledge based engineering techniques, pp 681-688.

VERMEULEN, B., EMBEREY, C.L., MILTON, N.R., VAN DER ELST, S.W.G and VAN TOOREN, M.J.L. Application of a knowledge based design methodology to support fuselage panel design, pp 589-597.

VISSER, H.G., HEBLY, S.J. and HARTJES, S. Optimisation of RNAV noise and emission abatement standard instrument departures, pp 757-767.

VITALE, A., GENITO, N., GARBARINO, L., CINIGLIO, U. and CORRARO, F. A hybrid frequency-time domain technique for ground effect identification, pp 377-385.

VOIT-NITCHMANN, R., SCHMOLLGRUBER, P., GOBERT, J.-L., GALL, P.-E., GORAJ, Z., JENTINK, H.W. and NAS, A. An innovative evaluation platform for new aircraft concepts, pp 451- 456.

VOSKUIJL, M., PADFIELD, G.D., WALKER, D.J., MANIMALA, B.J. and GUBBELS, A.W. Simulation of automatic helicopter deck landings using nature inspired flight control, pp 25-34.

WALKER, D.J., MANIMALA, B.J., GUBBELS, A.W., VOSKUIJL, M. and PADFIELD, G.D. Simulation of automatic helicopter deck landings using nature inspired flight control, pp 25-34.

WALKER, S.M., TAYLOR, G.K., CARRUTHERS, A.C. and THOMAS, A.L.R. Mechanics and aerodynamics of perching manoeuvres in a large bird of prey, pp 673-680.

WANG, J. and BAKER, A. Aspects of battle damage repair