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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 of helicopter structures, pp 321-332. 


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


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


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


WINARTO, H. and KHURANA, M. 
Development and validation of an efficient direct numerical optimization 
approach for aerofoil shape design, pp 61 1-628. 


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


ZACHOS, P.K. and KALFAS, A.1. 
Analysis of turbine performance degradation effects due to geometry 
variations between actual components and design intent, pp 569-578. 


ZAHIR, S., KHAN, M.A. and SAMAR, R. 
Flight control using pin-protuberances for blunted cones, pp 245-257. 


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


Volume CXIV 


Number 1151 January 


Number 1152 February 
Number 1153 March 
Number 1154 April 
Number 1155 May 
Number 1156 June 
Number 1157 July 
Number 1158 August 
Number 1159 September 
Number 1160 October 
Number 1161 
Number 1162 


November 
December 


pp 1-59 

pp 61-123 
pp 125-207 
pp 209-279 
pp 281-343 
pp 345-403 
pp 405-457 
pp 459-525 
pp 527-597 
pp 599-656 
pp 659-713 
pp 715-797