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THE AERONAUTICAL JOURNAL 


THE AERONAUTICAL JOURNAL 


OF THE ROYAL AERONAUTICAL SOCIETY 


Volume CIX 


January-December 2005 


Subject Index 


ACOUSTICS 

Acoustic validation of a new code using particle wake aerodynamics 
and geometrically-exact beam structural dynamics. F. Nitzsche 
and D.G. Opoku, pp 257-267. 

Life before and after implementation of an acoustic noise reduction 
enclosure. B. Timmin, pp 65-74 

Prediction of acoustic resonance phenomena for cavities using 
detached eddy simulations. R.M. Ashworth, pp 631-638. 


AERODYNAMICS 

Technical Note: A theoretical description of viscous flow along a 
flat plate. R.C. Hastings, pp 585-589. 

Effects of leading-edge bevel angle on the aerodynamic forces of a 
non-slender 50° delta wing. J.J. Wang and S.F. Lu, pp 403-407. 

Kite performance testing by flying in a circle. J. Stevenson, K. 
Alexander and P. Lynn, pp 269-276. 

Status and perspectives of laminar flow. G. Schrauf, pp 639-644. 


AEROELASTICITY 

Acoustic validation of a new code using particle wake aerodynamics 
and geometrically-exact beam structural dynamics. F. Nitzsche 
and D.G. Opoku, pp 257-267 

High-fidelity computational simulation of nonlinear fluid-structure 
interactions. R.E. Gordnier and M.R. Visbal, pp 301-312. 

Low frequency behaviour of the subsonic doublet lattice method. L. 
van Zyl, pp 285-291. 

Modelling and vibration of thin-walled rotating composite blades 
featuring extension-twist elastic coupling. S-Y. Oh, L. Librescu 
and O. Song, pp 233-246. 

Polynomial series expansion for optimisation of wing plane structures 
in idealised critical flutter conditions. S. Tizzi, pp 23-33. 


AEROSPACE ENGINEERING 

Design and structural analysis of a thrust chamber for a spinning 
supersonic rocket — a case study. K.M. Rajan and K. Narasimhan, 
pp 187-192. 

Jet thrust vectoring using a miniature fluidic oscillator. G. Raman, S. 
Packiarajan, G. Papadopoulos, C. Weissman and S. Raghu, pp 
129-138. 

Solar-powered space flight. M.H.D. Kemp, pp 619-670. 


AIR TRAFFIC MANAGEMENT 

Equipment failures in ATC: Finding an appropriate safety target. B. 
Subotic, W. Ochieng and A. Majumdar, pp 277-284. 

Semi-optimal co-ordinated manoeuvres for aircraft conflict 
resolution. J. Parastari and M.B. Malaek, pp 313-323. 

Studies of capacity estimation of the airport with two parallel 
runways. Y. Cao, Y. Chen and Y. Zhou, pp 395-401. 


BOOK REVIEWS - BY AUTHOR 

Ashby, M.F. and Jones, D.R.H. Engineering Materials 1: an Introduction 
to Properties, Applications and Design — Third edition, p 390. 

Baker, A. et al (Ed) Composite Materials for Aircraft Structures 
Second edition, p 417. 

Barton, D.K. Radar System Analysis and Modeling, p 391. 

Batra, R.C. Elements of Continuum Mechanics, p 391. 

Cumpsty, N. Jet Propulsion: a simple guide to the aerodynamic and 
thermodynamic design and performance of jet engines — Second 
edition, p 358. 

Curry, G.R. Radar System Performance Modeling — Second edition, 
p 391. 

Driels, M.R. Weaponeering: Conventional Weapon System 
Effectiveness, p 200. 





646 THE AERONAUTICAL JOURNAL 


Gutman, S. Applied Min-Max Approach to Missile Guidance and 
Control. Progress in Astronautics and Aeronautics series — Vol 
209, p 418. 

Hosford, W.F. Mechanical Behaviour of Materials, p 390. 

Howe, D. Aircraft Loading and Structural Layout, p 200. 

Jones, D.R.H. and Ashby, M.F. Engineering Materials 1: an 
Introduction to Properties, Applications and Design — Third 
edition, p 391. 

Reddy, A.V. Investigation of Aeronautical and Engineering 
Component Failures, p 358. 

Stengel, R.F. Flight Dynamics, p 417. 

Taylor, J.R. Classical Mechanics, p 201. 


BOOK REVIEWS - BY TITLE 

Aircraft Loading and Structural Layout, D. Howe, p 200. 

Applied Min-Max Approach to Missile Guidance and Control. 
Progress in Astronautics and Aeronautics series — Vol 209, S. 
Gutman, p 418. 

Classical Mechanics, J.R. Taylor, p 201. 

Composite Materials for Aircraft Structures — Second edition, A. 
Baker ef a/ (Editor), p 417. 

Elements of Continuum Mechanics, R.C. Batra, p 391. 

Engineering Materials |: an Introduction to Properties, Applications 
and Design — Third edition, M.F. Ashby and D.R.H. Jones, p 390. 

Flight Dynamics, R.F. Stengel, p 417. 

Investigation of Aeronautical and Engineering Component Failures, 
A.V. Reddy, p 358. 

Jet Propulsion: a simple guide to the aerodynamic and 
thermodynamic design and performance of jet engines — Second 
edition, N. Cumpsty, p 358. 

Mechanical Behaviour of Materials, W.F. Hosford, p 390. 

Radar System Analysis and Modeling, D.K. Barton, p 391. 


9 

Radar System Performance Modeling — Second edition, G.R. Curry, 
p 391. 

Weaponeering: Conventional Weapon System Effectiveness, M.R. 
Driels, p 200. 


COMPOSITES 

Design of composite helicopter rotor blades to meet given cross- 
sectional properties. S.L. Lemanski, P.M. Weaver, G.F.J. Hill, pp 
471-475. 

Modelling and vibration of thin-walled rotating composite blades 
featuring extension-twist elastic coupling. S-Y. Oh, L. Librescu 
and O. Song, pp 233-246. 

COMPUTATIONAL FLUID DYNAMICS 

Computational fluid dynamics study of unconventional air vehicle 
configurations. R. Ramamurti, W. Sandberg, P. Vaiana, J. Kellogg 
and D. Cylinder, pp 337-347. 

Evaluation of CFD methods for transport aircraft high lift systems. 
R. Rudnik, P. Eliasson and J. Perraud, pp 53-64. 

Numerical simulation of rim seal flows in axial turbines. J. Boudet, 
V.N.D. Autef, J.W. Chew, N.J. Hills and O. Gentilhomme, pp 
373-383. 

Progress toward CFD for full flight envelope. E.N. Tinoco, D.R. 
Bogue, T-J. Kao, N.J. Yu, P. Li and D.N. Ball, pp 451-460. 


COMPUTATIONAL TECHNIQUES (GENERAL) 

A numerical study on the mixing of air and hydrogen in a scramjet 
combustor. M. Ali and T. Fujiwara, pp 325-335. 

Application of Java and VRML visualisation tools in store release 
wind-tunnel testing. D.M. Orchard, M. Ahmadi and F.C. Tang, pp 
569-576. 

High-fidelity computational simulation of nonlinear fluid-structure 
interactions. R.E. Gordnier and M.R. Visbal, pp 301-312. 

Neuro-fuzzy approach for performance optimisation of variable 
nozzle turbofan engine. T.R. Nada and A.A. Hashem, pp 139-146. 

DEFENCE 


DECEMBER 2005 


Flight control system damage simulation using freely flying models. 
S. Sadovnychiy, A. Ryzhenko and A. Betin, pp 45-50. 


DESIGN 

Bio-inspired design of flapping-wing micro air vehicles. K.D. Jones, 
C.J. Bradshaw, J. Papadopoulos and M.F. Platzer, pp 385-393. 

Development of an airship for tropical rain forest canopy 
exploration. G.E. Dorrington, pp 361-372. 


ENVIRONMENTAL ENGINEERING 

Air Travel — Greener by Design Mitigating the environmental 
impact of aviation: Opportunities and priorities. J.E Green, pp 
361-416. 

Erratum: Greener by Design — The technology challenge. J.E. 
Green, pp 98-99. 


FLIGHT CONTROL 

Collision avoidance within flight dynamics constraints for UAV 
applications. R.W. Penney, pp 193-199. 

Dynamic gain-scheduled control of the ICE 101-TV. T.S. 
Richardson, M.H. Lowenburg and C.D.C. Jones, pp 593-607. 

Flight control system damage simulation using freely flying models. 
S. Sadovnychiy, A. Ryzhenko and A. Betin, pp 45-50. 

Semi-optimal co-ordinated manoeuvres for aircraft conflict 
resolution. J. Parastari and M.B. Malaek, pp 313-323. 

Simulation and flight test of a temperature sensing stabilisation 
system. P. Herrmann and C. Bil, pp 167-175. 

The birth of the practical aeroplane: An appraisal of the Wright 
brothers’ achievements. G.D. Padfield and B. Lawrence, pp 421-437. 


FLIGHT SIMULATION 
Integrated design of flight simulator motion cueing systems. R. 
Hosman, S. Advani and N. Haeck, p 1. 


HISTORY 
The birth of the practical aeroplane: An appraisal of the Wright 
brothers’ achievements. G.D. Padfield and B. Lawrence, pp 421-437. 


HUMAN FACTORS 
A novel approach to encouraging proper fatigue management in British 
Army aviation training and operations. R.P. King, pp 293-298. 


INDUSTRY 
Trade disputes in the commercial aircraft industry: A background 
note. K. Hayward, pp 157-166. 


JETS 

2D numerical study of circular synthetic jets in quiescent flows. H. 
Tang and S. Zhong, pp 89-97. 

Dye visualisation of inclined and skewed synthetic jets in a cross 
flow. S. Zhong, L. Garcillan and N.J Wood, pp 147-155. 

Industry applications of advanced flow diagnostics experience in the 
BAE Systems ground effects rig. P. Curtis, pp 119-127. 

Investigation into clustering of synthetic jet actuators. S.C. Liddle 
and N.J. Wood, pp 35-44. 

PIV measurements in a twin-jet STOVL fountain flow. P.M. 
Cabrita, A.J. Saddington and K. Knowles, pp 439-449. 

The behaviour of circular synthetic jets in a laminar boundary layer. 
S. Zhong, F. Millet, and N.J. Wood, pp 461-470. 


LIGHTER THAN AIR 
Development of an airship for tropical rain forest canopy 
exploration. G.E. Dorrington, pp 361-372. 


PROPULSION 

A numerical study on the mixing of air and hydrogen in a scramjet 
combustor. M. Ali and T. Fujiwara, pp 

Comprehensive validation of an intermittency transport model for 





INDEX TO VOLUME 109 647 


transitional low-pressure turbine flows. Y.B. Suzen and P.G. 
Huang, pp 101-118. 

Design and structural analysis of a thrust chamber for a spinning 
supersonic rocket — a case study. K.M. Rajan and K. Narasimhan, 
pp 187-192. 

Infra-red signature reduction study on a small-scale jet engine. J. Dix, 
A.J. Saddington, K. Knowles and M.A. Richardson, pp 83-88. 

Jet thrust vectoring using a miniature fluidic oscillator. G. Raman, S. 
Packiarajan, G. Papadopoulos, C. Weissman and S. Raghu, pp 
129-138. 

Limited life engines for UAVs. I.K. Clark, pp 247-254. 

Neuro-fuzzy approach for performance optimisation of variable 
nozzle turbofan engine. T.R. Nada and A.A. Hashem, pp 139-146. 

Numerical simulation of rim seal flows in axial turbines. J. Boudet, 
V.N.D. Autef, J.W. Chew, N.J. Hills and O. Gentilhomme, pp 
373-383. 

Solar-powered space flight. M.H.D. Kemp, pp 619-670. 


ROTORCRAFT 

Acoustic validation of a new code using particle wake aerodynamics 
and geometrically-exact beam structural dynamics. F. Nitzsche 
and D.G. Opoku, pp 257-267. 

Design of composite helicopter rotor blades to meet given cross- 
sectional properties. S.L. Lemanski, P.M. Weaver, G.F.J. Hill, pp 
471-475. 


SAFETY 

A civil aviation safety assessment model using a Bayesian belief 
network (BBN). R. Greenberg, S.C. Cook and D. Harris, pp 557- 
568. 

A novel approach to encouraging proper fatigue management in British 
Army aviation training and operations. R.P. King, pp 293-298. 

Equipment failures in ATC: Finding an appropriate safety target. B. 
Subotic, W. Ochieng and A. Majumdar, pp 277-284. 

Semi-optimal co-ordinated manoeuvres for aircraft conflict 
resolution. J. Parastari and M.B. Malaek, pp 313-323. 


SHOCK WAVES 

Experiments on the hypersonic turbulent shock-wave/boundary- 
layer interaction and the effects of surface roughness. S.A. Prince, 
M. Vannahme and J.L. Stollery, pp 177-185 

Normal shock wave/turbulent boundary-layer interaction control 
using ‘smart’ piezoelectric actuators. J.S. Couldrick, S.L. Gai, J.F. 
Milthorpe and K. Shankar, pp 577-583. 

Shock-wave induced instability in internal explosion dynamics. A. 
Bagabir and D. Drikakis, pp 537-556. 


STRUCTURES 

Design and structural analysis of a thrust chamber for a spinning 
supersonic rocket — a case study. K.M. Rajan and K. Narasimhan, 
pp 187-192. 

Optimum design for buckling of arbitrary shaped ribs under 
uncertain loads. A.C. Conrado, A.R. de Faria and S.F.M. de 
Almeida, pp 609-618. 


TESTING FACILITIES AND TECHNIQUES 

Application of Java and VRML visualisation tools in store release 
wind-tunnel testing. D.M. Orchard, M. Ahmadi and F.C. Tang, pp 
569-576. 

Experimental investigation of the effect of nozzle shape and test 
section perforation on the stationary and non-stationary 
characteristics. V.I. Biryukov, S.A. Glazkov, A.R. Gorbushin, A.1. 
Ivanov and A.V. Semenov, pp 75-82. 

Industry applications of advanced flow diagnostics experience in the 
BAE Systems ground effects rig. P. Curtis, pp 119-127. 

Kite performance testing by flying in a circle. J. Stevenson, K. 
Alexander and P. Lynn, pp 269-276. 

Utilising flight test telemetry data to improve store trajectory 


simulations. A.T. Cenko, A.G. Piranian and S. Denihan, pp 349- 


Be 20 2 


UNMANNED AIR VEHICLES 

Bio-inspired design of flapping-wing micro air vehicles. K.D. Jones, 
C.J. Bradshaw, J. Papadopoulos and M.F. Platzer, pp 385-393. 

Collision avoidance within flight dynamics constraints for UAV 
applications. R.W. Penney, pp 193-199. 

Computational fluid dynamics study of unconventional air vehicle 
configurations. R. Ramamurti, W. Sandberg, P. Vaiana, J. Kellogg 
and D. Cylinder, pp 337-347. 

Limited life engines for UAVs. I.K. Clark, pp 247-254. 

Simulation and flight test of a temperature sensing stabilisation 
system. P. Herrmann and C. Bil, pp 167-175. 


UNSTEADY AERODYNAMICS 

A review of some recent developments in flow control. P.R. Ashill, 
J.L. Fulker and K.C. Hackett, pp 205-232. 

Experiments on the hypersonic turbulent shock-wave/boundary- 
layer interaction and the effects of surface roughness. S.A. Prince, 
M. Vannahme and J.L. Stollery, pp 177-185. 

Low frequency behaviour of the subsonic doublet lattice method. L. 
van Zyl, pp 285-291. 

Normal shock wave/turbulent boundary-layer interaction control 
using ‘smart’ piezoelectric actuators. J.S. Couldrick, S.L. Gai, J.F. 
Milthorpe and K. Shankar, pp 577-583. 

PIV measurements in a twin-jet STOVL fountain flow. P.M. 
Cabrita, A.J. Saddington and K. Knowles, pp 439-449. 

Progress toward CFD for full flight envelope. E.N. Tinoco, D.R. 
Bogue, T-J. Kao, N.J. Yu, P. Li and D.N. Ball, pp 451-460. 


VIBRATION 

Acoustic validation of a new code using particle wake aerodynamics 
and geometrically-exact beam structural dynamics. F. Nitzsche 
and D.G. Opoku, pp 257-267. 

Modelling and vibration of thin-walled rotating composite blades 
featuring extension-twist elastic coupling. S-Y. Oh, L. Librescu 
and O. Song, pp 233-246. 


WAKES 

Comprehensive validation of an intermittency transport model for 
transitional low-pressure turbine flows. Y.B. Suzen and P.G. 
Huang, pp 101-118. 

The vortex merger factor in aircraft wake turbulence. M. Mokry, pp 

13-22. 


5 





THE AERONAUTICAL JOURNAL 


DECEMBER 2005 


Author Index 


ADVANI, S., HAECK, N. and HOSMAN, R. 
Integrated design of flight simulator motion cueing systems, p 1. 


AHMADI, M., TANG, F.C. and ORCHARD, D.M. 
Application of Java and VRML visualisation tools in store release 
wind-tunnel testing, pp 569-576. 


ALEXANDER, K., LYNN, P. and STEVENSON, J. 


Kite performance testing by flying in a circle, pp 269-276. 


ALI, M. and FUJIWARA, T. 
A numerical study on the mixing of air and hydrogen in a scramjet 


DE ALMEIDA, S.F.M., CONRADO, A.C. and DE FARIA, A.R. 


Optimum design for buckling of arbitrary shaped ribs under 
uncertain loads, pp 609-618. 


ASHILL, P.R., FULKER, J.L. and HACKETT, K.C. 


A review of some recent developments in flow control, pp 205-232. 


ASHWORTH, R.M. 
Prediction of acoustic resonance phenomena for cavities using 
detached eddy simulations, pp 631-638. 


AUTEF, V.N.D., CHEW, J.W., HILLS, N.J., GENTILHOMME, O. 


and BOUDET, J. 
Numerical simulation of rim seal flows in axial turbines, pp 373- 


383. 


BAGABIR, A. and DRIKAKIS, D. 
Shock-wave induced instability in internal explosion dynamics, pp 


537-556. 
BALL, D.N., TINOCO, E.N., BOGUE, D.R., KAO, T-J., YU, N.J. 
and LI, P. 


Progress toward CFD for full flight envelope, pp 451-460. 


BETIN, A, SADOVNYCHIY, S. and RYZHENKO, A. 


Flight control system damage simulation using freely flying models, 


pp 45-50. 


BETIN, A., SADOVNYCHIY, S. and RYZHENKO, A. 


Flight control system damage simulation using freely flying models, 


pp 45-50. 


BIL, C. and HERRMANN, P. 
Simulation and flight test of a temperature sensing stabilisation 
system, pp 167-175. 


BIRYUKOV, V.1., GLAZKOV, S.A., GORBUSHIN, A.R., 
IVANOV, A.I. and SEMENOV, A.V. 

Experimental investigation of the effect of nozzle shape and test 
section perforation on the stationary and non-stationary 
characteristics, pp 75-82. 


BOGUE, D.R., KAO, T-J., YU, N.J., LI, P., BALL, D.N. and 
TINOCO, E.N. 
Progress toward CFD for full flight envelope, pp 451-460. 


BOUDET, J., AUTEF, V.N.D., CHEW, J.W., HILLS, N.J. and 
GENTILHOMME, O. 
Numerical simulation of rim seal flows in axial turbines, pp 373-383. 


BRADSHAW, C.J., PAPADOPOULOS, J., PLATZER, M.F. 
and JONES, K.D. 


Bio-inspired design of flapping-wing micro air vehicles, pp 385-393. 


CABRITA, P.M., SADDINGTON, A.J. and KNOWLES, K. 
PIV measurements in a twin-jet STOVL fountain flow, pp 439-449. 


CAO, Y., CHEN, Y. and ZHOU, Y. 
Studies of capacity estimation of the airport with two parallel 
runways, pp 395-401. 


CENKO, A.T., PIRANIAN, A.G. and DENIHAN, S. 
Utilising flight test telemetry data to improve store trajectory 
simulations, pp 349-357. 


CHEN, Y., ZHOU, Y. and CAO, Y. 
Studies of capacity estimation of the airport with two parallel 
runways, pp 395-401. 


CHEW, J.W., HILLS, N.J., GENTILHOMME, O., BOUDET, J. 
and AUTEF, V.N.D. 
Numerical simulation of rim seal flows in axial turbines, pp 373-383. 


CLARK, I.K. 


Limited life engines for UAVs, pp 247-254. 


CONRADO, A.C., DE FARIA, A.R. and DE ALMEIDA, S.F.M. 
Optimum design for buckling of arbitrary shaped ribs under 
uncertain loads, pp 609-618. 


COOK, S.C., HARRIS, D. and GREENBERG, R. 
A civil aviation safety assessment model using a Bayesian belief 
network (BBN), pp 557-568. 


COULDRICK, J.S., GAI, S.L., MILTHORPE, J.F. and 
SHANKAR, K. 

Normal shock wave/turbulent boundary-layer interaction control 
using ‘smart’ piezoelectric actuators, pp 577-583. 


CURTIS, P. 
Industry applications of advanced flow diagnostics experience in the 
BAE Systems ground effects rig, pp 119-127. 


CYLINDER, D., RAMAMURTI, R., SANDBERG, W., 
VAIANA, P. and KELLOGG, J. 

Computational fluid dynamics study of unconventional air vehicle 
configurations, pp 337-347. 





INDEX TO VOLUME 109 


DENIHAN, S., CENKO, A.T. and PIRANIAN, A.G. 
Infra-red signature reduction study on a small-scale jet engine, pp 
83-88. 


DIX, J.. SADDINGTON, A.J., KNOWLES, K. and 
RICHARDSON, M.A. 

Development of an airship for tropical rain forest canopy 
exploration, pp 361-372. 


DORRINGTON, G.E. 
Shock-wave induced instability in internal explosion dynamics, pp 
537-556. 


DRIKAKIS, D. and BAGABIR, A. 
Evaluation of CFD methods for transport aircraft high litt systems, 
pp 53-64. 


ELIASSON, P, PERRAUD, J. and RUDNIK, R. 
Optimum design for buckling of arbitrary shaped ribs under 
uncertain loads, pp 609-618. 


DE FARIA, A.R., DE ALMEIDA, S.F.M. and CONRADO, A.C. 


Utilising flight test telemetry data to improve store trajectory 
simulations, pp 349-357. 


FUJIWARA, T. and ALI, M. 
A numerical study on the mixing of air and hydrogen in a scramjet 


combustor, pp 325-335. 


FULKER, J.L., HACKETT, K.C. and ASHILL, P.R 


A review of some recent developments in flow control, pp 205- 


23 


a 

GAI, S.L., MILTHORPE, J.F., SHANKAR, K. and 
COULDRICK, JS. 

Normal shock wave/turbulent boundary-layer interaction control 


using 'smart' piezoelectric actuators, pp 577-583 


GARCILLAN, L., WOOD, N.J and ZHONG, S. 
Dye visualisation of inclined and skewed synthetic jets in a cross 
flow, pp 147-155. 


GENTILHOMME, O., BOUDET, J., AUTEF, V.N.D., CHEW, 
J.W. and HILLS, N.J. 


Numerical simulation of rim seal flows in axial turbines, pp 373-383. 


GLAZKOV, S.A., GORBUSHIN, A.R., IVANOV, A.L, 
SEMENOV, A.V. and BIRYUKOYV, V.I. 

Experimental investigation of the effect of nozzle shape and test 
section perforation on the stationary and non-stationary 
characteristics, pp 75-82. 


GORBUSHIN, A.R., IVANOV, A.L, SEMENOV, A.V., 
BIRYUKOV, V.I. and GLAZKOV, S.A. 

Experimental investigation of the effect of nozzle shape and test 
section perforation on the stationary and non-stationary 
characteristics, pp 75-82. 


GORDNIER, R.E. and VISBAL, M.R. 
High-fidelity computational simulation of nonlinear fluid-structure 
interactions, pp 301-312. 


GREEN, J.E. 

Air Travel — Greener by Design Mitigating the environmental 
impact of aviation: Opportunities and priorities, pp 361-416. 

Erratum: Greener by Design — The technology challenge, pp 98-99. 


GREENBERG, R., COOK, S.C. and HARRIS, D. 
A civil aviation safety assessment model using a Bayesian belief 
network (BBN), pp 557-568 


HACKETT, K.C., ASHILL, P.R. and FULKER, J.L. 


A review of some recent developments in flow control, pp 205-232. 


HAECK, N., HOSMAN, R. and ADVANI, S. 


Integrated design of flight simulator motion cueing systems, p 1. 


HARRIS, D., GREENBERG, R. and COOK, S.C. 
A civil aviation safety assessment model using a Bayesian belief 
network (BBN), pp 557-568. 


HASHEM, A.A. and NADA, T.R. 
Neuro-fuzzy approach for performance optimisation of variable 
nozzle turbofan engine, pp 139-146. 


HASTINGS, R.C. 
Technical Note: A theoretical description of viscous flow along a 
flat plate, pp 585-589. 


HAYWARD, K. 
Trade disputes in the commercial aircraft industry: A background 
note, pp 157-166. 


HERRMANN, P. and BIL, C. 
Simulation and flight test of a temperature sensing stabilisation 
system, pp 167-175. 


HILL, G.F.J., LEMANSKI, S.L. and WEAVER, P.M. 
Design of composite helicopter rotor blades to meet given cross- 
sectional properties, pp 471-475. 


HILLS, N.J., GENTILHOMME, O., BOUDET, J., AUTEF, 
V.N.D. and CHEW, J.W. 
Numerical simulation of rim seal flows in axial turbines, pp 373- 


383. 


HOSMAN, R., ADVANI, S. and HAECK, N. 


Integrated design of flight simulator motion cueing systems, p 1. 


HUANG, P.G. and SUZEN, Y.B. 
Comprehensive validation of an intermittency transport model for 
transitional low-pressure turbine flows, pp 101-118. 


IVANOV, A.I., SEMENOV, A.V., BIRYUKOV, V.L., 
GLAZKOV, S.A. and GORBUSHIN, A.R. 

Experimental investigation of the effect of nozzle shape and test 
section perforation on the stationary and non-stationary 
characteristics, pp 75-82. 


JONES, C.D.C., RICHARDSON, T.S. and LOWENBURG, 
M.H. 
Dynamic gain-scheduled control of the ICE 101-TV, pp 593-607. 





650 THE AERONAUTICAL JOURNAL 


JONES, K.D., BRADSHAW, C.J., PAPADOPOULOS, J. and 
PLATZER, M.F. 


Bio-inspired design of flapping-wing micro air vehicles, pp 385-393. 


KAO, T-J., YU, N.J., LI, P., BALL, D.N.TINOCO, E.N. and 
BOGUE, D.R. 
Progress toward CFD for full flight envelope, pp 451-460. 


KELLOGG, J., CYLINDER, D-RAMAMURTI, R., 
SANDBERG, W. and VAIANA, P. 

Computational fluid dynamics study of unconventional air vehicle 
configurations, pp 337-347. 


KEMP, M.H.D. 


Solar-powered space flight, pp 619-670. 


KING, R.P. 
A novel approach to encouraging proper fatigue management in 
British Army aviation training and operations, pp 293-298. 


KNOWLES, K., CABRITA, P.M. and SADDINGTON, A.J. 
Infra-red signature reduction study on a small-scale jet engine, pp 
83-88. 


KNOWLES, K., RICHARDSON, M.A., DIX, J. and 
SADDINGTON, A.J. 
PIV measurements in a twin-jet STOVL fountain flow, pp 439-449 


LAWRENCE, B. and PADFIELD, G.D. 
The birth of the practical aeroplane: An appraisal of the Wright 
brothers’ achievements, pp 421-437. 


LEMANSKI, S.L., WEAVER, P.M. and HILL, G.F.J. 
Design of composite helicopter rotor blades to meet given cross- 
sectional properties, pp 471-475. 


LI, P., BALL, D.N., TINOCO, E.N., BOGUE, D.R., KAO, T-J. 
AND YU,N.J. 


Progress toward CFD for full flight envelope, pp 451-460. 


LIBRESCU, L., SONG, O. and OH, S-Y. 
Modelling and vibration of thin-walled rotating composite blades 
featuring extension-twist elastic coupling, pp 233-246. 


LIDDLE, S.C. and WOOD, N.J. 


Investigation into clustering of synthetic jet actuators, pp 35-44. 


LOWENBURG, M.H., JONES, C.D.C. and RICHARDSON, 
T.S. 


Dynamic gain-scheduled control of the ICE 101-TV, pp 593-607. 
LU, S.F. and WANG, J.J. 
Effects of leading-edge bevel angle on the aerodynamic forces of a 


non-slender 50° delta wing, pp 403-407. 


LYNN, P., STEVENSON, J. and ALEXANDER, K. 
Kite performance testing by flying in a circle, pp 269-276. 


MAJUMDAR, A., SUBOTIC, B. and OCHIENG, W. 


Equipment failures in ATC: Finding an appropriate safety target, pp 
277-284. 


DECEMBER 2005 


MALAEK, M.B. and PARASTARI, J. 
Semi-optimal co-ordinated manoeuvres for aircraft conflict 
resolution, pp 313-323. 


MILLET, F., WOOD, N.J. and ZHONG, S. 
The behaviour of circular synthetic jets in a laminar boundary layer, 
pp 461-470. 


MILTHORPE, J.F., SHANKAR, K., COULDRICK, J.S. and 
GAT, S.L. 

Normal shock wave/turbulent boundary-layer interaction control 
using ‘smart’ piezoelectric actuators, pp 577-583. 


MOKRY, M. 


The vortex merger factor in aircraft wake turbulence, pp 13-22. 


NADA, T.R. and HASHEM, A.A. 
Neuro-fuzzy approach for performance optimisation of variable 
nozzle turbofan engine, pp 139-146. 


NARASIMHAN, K. and RAJAN, K.M. 
Design and structural analysis of a thrust chamber for a spinning 
supersonic rocket — a case study, pp 187-192. 


NITZSCHE, F. and OPOKU, D.G. 

Acoustic validation of a new code using particle wake 
aerodynamics and geometrically-exact beam structural 
dynamics, pp 257-267. 


OCHIENG, W., MAJUMDAR, A. and SUBOTIC, B. 
Equipment failures in ATC: Finding an appropriate safety target, pp 
277-284. 


OH, S-Y., LIBRESCU, L. and SONG, O. 
Modelling and vibration of thin-walied rotating composite blades 
featuring extension-twist elastic coupling, pp 233-246. 


OPOKU, D.G. and NITZSCHE, F. 

Acoustic validation of a new code using particle wake 
aerodynamics and geometrically-exact beam structural 
dynamics, pp 257-267. 


ORCHARD, D.M., AHMADI, M. and TANG, F.C. 
Application of Java and VRML visualisation tools in store release 
wind-tunnel testing, pp 569-576. 


PACKIARAJAN, S., PAPADOPOULOS, G., WEISSMAN, C., 
RAGHU, S. and RAMAN, G. 
Jet thrust vectoring using a miniature fluidic oscillator, pp 129-138. 


PADFIELD, G.D. and LAWRENCE, B. 
The birth of the practical aeroplane: An appraisal of the Wright 
brothers’ achievements, pp 421-437. 


PAPADOPOULOS, G., WEISSMAN, C, RAGHU, S,.RAMAN, 
G. and PACKIARAJAN, S. 
Jet thrust vectoring using a miniature fluidic oscillator, pp 129-138. 


PAPADOPOULOS, J., PLATZER, M.F., JONES, K.D. and 
BRADSHAW, C.J. 
Bio-inspired design of flapping-wing micro air vehicles, pp 385-393. 





INDEX TO VOLUME 109 


PARASTARI, J. and MALAEK, M.B. 
Semi-optimal co-ordinated manoeuvres for aircraft conflict 
resolution, pp 313-323. 


PENNEY, R.W. 
Collision avoidance within flight dynamics constraints for UAV 
applications, pp 193-199. 


PERRAUD, J., RUDNIK, R. and ELIASSON, P. 
Evaluation of CFD methods for transport aircraft high lift systems, 
pp 53-64. 


PIRANIAN, A.G., DENIHAN, S. and CENKO, A.T. 
Utilising flight test telemetry data to improve store trajectory 
simulations, pp 349-357. 


PLATZER, M.F., JONES, K.D., BRADSHAW, C.J. and 
PAPADOPOULOS, J. 


Bio-inspired design of flapping-wing micro air vehicles, pp 385-393. 


PRINCE, S.A., VANNAHME, M. and STOLLERY, J.L. 
Experiments on the hypersonic turbulent shock-wave/boundary- 
layer interaction and the effects of surface roughness, pp 177-185. 


RAGHU, S., RAMAN, G., PACKIARAJAN, S., 
PAPADOPOULOS, G. and WEISSMAN, C. 


Jet thrust vectoring using a miniature fluidic oscillator, pp 129-138. 


RAJAN, K.M. and NARASIMHAN, K. 
Design and structural analysis of a thrust chamber for a spinning 
supersonic rocket — a case study, pp 187-192 


RAMAMURTI, R., SANDBERG, W., VAIANA, P., KELLOGG, 
J. and CYLINDER, D. 

Computational fluid dynamics study of unconventional air vehicle 
configurations, pp 337-347. 


RAMAN, G., PACKIARAJAN, S., PAPADOPOULOS, G., 
WEISSMAN, C. and RAGHU, S. 
Jet thrust vectoring using a miniature fluidic oscillator, pp 129-138. 


RICHARDSON, M.A., DIX, J., SADDINGTON, A.J. and 
KNOWLES, K. 

Infra-red signature reduction study on a small-scale jet engine, pp 
83-88. 


RICHARDSON, T.S., LOWENBURG, M.H. and JONES, 
C.D.C. 
Dynamic gain-scheduled control of the ICE 101-TV, pp 593-607. 


RUDNIK, R., ELIASSON, P. and PERRAUD, J. 
Evaluation of CFD methods for transport aircraft high lift systems, 
pp 53-64. 


SADDINGTON, A.J., KNOWLES, K. and CABRITA, P.M. 
PIV measurements in a twin-jet STOVL fountain flow, pp 439-449. 


SADDINGTON, A.J., KNOWLES, K. and RICHARDSON, 
M.A. and DIX, J. 


Infra-red signature reduction study on a small-scale jet engine, pp 
83-88. 


SADOVNYCHIY, S., RYZHENKO, A. and BETIN, A. 
Flight control system damage simulation using freely flying models, 
pp 45-50. 


SANDBERG, W., VAIANA, P., KELLOGG, J., CYLINDER, D. 
and RAMAMURTIL, R. 

Computational fluid dynamics study of unconventional air vehicle 
configurations, pp 337-347. 


SCHRAUF, G. 
Status and perspectives of laminar flow, pp 639-644. 


SEMENOV, A.V., BIRYUKOV, V.I., GLAZKOV, S.A., 
GORBUSHIN, A.R. and IVANOV, A.L. 

Experimental investigation of the effect of nozzle shape and test 
section perforation on the stationary and non-stationary 


characteristics, pp 75-82. 


SHANKAR, K., COULDRICK, J.S., GAI, S.L. and 
MILTHORPE, J.F. 

Normal shock wave/turbulent boundary-layer interaction control 
using ‘smart’ piezoelectric actuators, pp 577-583. 


SONG, O., OH, S-Y. and LIBRESCU, L. 

Modelling and vibration of thin-walled rotating composite blades 
featuring extension-twist elastic coupling, pp 233-246. 

STEVENSON, J., ALEXANDER, K. and LYNN, P. 

Kite performance testing by flying in a circle, pp 269-276. 


STOLLERY, J.L., PRINCE, S.A. and VANNAHME, M. 
Experiments on the hypersonic turbulent shock-wave/boundary- 
layer interaction and the effects of surface roughness, pp 177-185. 


SUBOTIC, B., OCHIENG, W. and MAJUMDAR, A. 
Equipment failures in ATC: Finding an appropriate safety target, pp 


277-284. 


SUZEN, Y.B. and HUANG, P.G. 
Comprehensive validation of an intermittency transport model for 
transitional low-pressure turbine flows, pp 101-118. 


TANG, F.C., ORCHARD, D.M. and AHMADI, M. 
Application of Java and VRML visualisation tools in store release 
wind-tunnel testing, pp 569-576. 


TANG, H. and ZHONG, S. 
2D numerical study of circular synthetic jets in quiescent flows, pp 
89-97. 


TIMMIN, B. 
Life before and after implementation of an acoustic noise reduction 
enclosure, pp 65-74. 


TINOCO, E.N., BOGUE, D.R., KAO, T-J., YU, N.J., LI, P. and 
BALL, D.N. 
Progress toward CFD for full flight envelope, pp 451-460. 


TIZZ1, S. 
Polynomial series expansion for optimisation of wing plane 
structures in idealised critical flutter conditions, pp 23-33. 





652 THE AERONAUTICAL JOURNAL 


VAIANA, P., KELLOGG, J., CYLINDER, D., RAMAMURTI, 
R. and SANDBERG, W. 

Computational fluid dynamics study of unconventional air vehicle 
configurations, pp 337-347. 


VAN ZYL, L. 
Experiments on the hypersonic turbulent shock-wave/boundary- 


layer interaction and the effects of surface roughness, pp 177-185. 


VANNAHME, M., STOLLERY, J.L. and PRINCE, S.A. 
High-fidelity computational simulation of nonlinear fluid-structure 
interactions, pp 301-312. 


VISBAL, M.R. and GORDNIER, R.E. 
Effects of leading-edge bevel angle on the aerodynamic forces of a 
non-slender 50° delta wing, pp 403-407. 


WANG, J.J. and LU, S.F. 
Design of composite helicopter rotor blades to meet given cross- 
sectional properties, pp 471-475. 


WEAVER, P.M., HILL, G.F.J. and LEMANSKI, S.L. 
Jet thrust vectoring using a miniature fluidic oscillator, pp 129-138. 


WEISSMAN, C., RAGHU, S. RAMAN, G., PACKIARAJAN, S., 


and PAPADOPOULOS, G. 
Dye visualisation of inclined and skewed synthetic jets in a cross 
flow, pp 147-155. 


WOOD, N.J, ZHONG, S. and GARCILLAN, L. 


Investigation into clustering of synthetic jet actuators, pp 35-44. 


WOOD, N.J. and LIDDLE, S.C. 
The behaviour of circular synthetic jets in a laminar boundary layer, 
pp 461-470. 


DECEMBER 2005 


WOOD, N.J., ZHONG, S. and MILLET, F. 
Progress toward CFD for full flight envelope, pp 451-460. 


YU, N.J., LI, P., BALL, D.N., TINOCO, E.N., BOGUE, D.R. and 
KAO, T-J. 

2D numerical study of circular synthetic jets in quiescent flows, pp 
89-97. 


ZHONG, S. and TANG, H. 
Dye visualisation of inclined and skewed synthetic jets in a cross 
flow, pp 147-155. 


ZHONG, S., GARCILLAN, L. and WOOD, N.J. 
The behaviour of circular synthetic jets in a laminar boundary layer, 
pp 461-470. 


ZHONG, S., MILLET, F. and WOOD, N.J. 
Studies of capacity estimation of the airport with two parallel 
runways, pp 395-401. 


ZHOU, Y., CAO, Y. and CHEN, Y. 


Low frequency behaviour of the subsonic doublet lattice method, pp 
285-291. 


Volume CIX 


Number 1091 January 
Number 1092 
Number 1093 


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1095 
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June 

July 
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pp 1-51 

pp 53-99 
pp 101-156 
pp 157-203 
pp 205-255 
pp 257-298 
pp 301-359 
pp 361-419 
pp 361-419 
pp 421-475 
pp 537-591 
pp 593-656 







































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