Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2004: Vol 218 Index

2004·0.7 MB·English

2004 Author Index
Armstrong, (¢ Weight reduction methodologies for a thrust reverser cascade using aerodynamic and
structural integration
Azzam, H Indirect approaches to individual aircraft structural monitoring
Balakrishnan, S Control of the wing rock motion using a new suboptimal control method
Bendiksen, O O Modern developments in computational aeroelasticity
Bharani, S Effect of angle-of-turn on the performance of divided intake ducts
Bismarck-Nasr, M N On the methodology of fitting design
Bonello, P rhe prediction of the non-linear dynamics of a squeeze-film damped aero-engine rotor
housed in a flexible support structure
Boni, | Development of analytical methods for fuselage design: validation by means of finite
element analyses
Brennan, M J rhe prediction of the non-linear dynamics of a squeeze-film damped aero-engine rotor
housed in a flexible support structure
Butterfield, J Weight reduction methodologies for a thrust reverser cascade using aerodynamic and
structural integration
aligiana, G Multiobjective wing design using genetic algorithms and fuzzy logic
ao, ¥ Numerical analysis of the airfoil flow fields and transonic blade — vortex interaction noise
hahl, JS An overview of insect-inspired guidance for application in ground and airborne
platforms
handramouli, R Effect of angle-of-turn on the performance of divided intake ducts
irci, ¢ Hybrid methods and Q-guidance for rocket performance optimization
lements, J A spacecraft attitude stabilization system with low-power magnetic torquers
ooper, J I Force appropriation for flight flutter testing
rowther, W J Rule-based guidance for flight vehicle flocking
unningham, P R A review of analytical methods for aircraft structures subjected to high-intensity random
acoustic loads
I Jesforges. M J Force appropriation for flight flutter testing
I llery, A An engineering approach to the dynamic control of space robotic on-orbit servicers
Ewins, D J State-of-the-art dynamic analysis for non-linear gas turbine structures
I anteria, D Development of anaiytical methods for fuselage design: validation by means of finite
element analyses
Frulla, G Aeroelastic behaviour of a solar-powered high-altitude long endurance unmanned air
vehicle (HALE-UAV) slender wing
Galinski, ¢ Some aeromechanical aspects of insect-like flapping wings in hover
Garratt, M An overview of insect-inspired guidance for application in ground and airborne
platforms
Gras, R Teeth clearance effects upon pressure and film thickness in a trochoidal hydrostatic gear
pump
Holmes, R rhe prediction of the non-linear dynamics of a squeeze-film damped aero-engine rotor
housed in a flexible support structure
Humphreys, B Liquid anti-contamination systems for hybrid laminar flow control aircraft — a review of
the critical issues and important experimental results
Ibrahim, J S Deformation analysis of aircraft wheels using a speckle shearing interferometer 287
lian, | The predicitve models of maintenance costs for a civil airplane 347
Kadebek, D A spacecraft attitude stabilization system with low-power magnetic torquers 99-109
Kang. P Numerical analysis of the airfoil flow fields and transonic blade — vortex interaction noise 125-131
Kim, J Decentralized approach to unmanned aerial vehicle navigation: without the use of the 399-416
global positioning system and preloaded maps
King, R | Non-linear simulation of coupled rotor — fuselage response using symbolically derived
equations of motion. Part |: derivation
King, R | Non-linear simulation of coupled rotor — fuselage response using symbolically derived
equations of motion. Part 2: confirmation and illustrative cases
Knowles, K Some aeromechanical aspects of insect-like flapping wings in hover
Lawson, N J [he application of laser measurement techniques to aerospace flows
Li, X Numerical analysis of the airfoil flow fields and transonic blade — vortex interaction noise
IMechE 2003 Proc. Instn Mech. Engrs Vol. 217 Part G: J. Aerospace Engineering
AUTHOR INDEX
Marczi, 1 ffect of number of ribs and spar load ratio on the wing mass for light aircraft 147-156
Mathioudakis, K Probabilistic neural networks for validation of on-board jet engine data $977
Mentch, D \ spacecraft attitude stabilization system with low-power magnetic torquers 99—109
Michelson, R ¢ Novel approachehes s to miniature flight platforms 363-37 >4
ized ap proach to unmanned aerial vehicle navigation: without the use of the 399-416
ing system and preloaded maps
ipproaches 399
ilized approach ti ¢ to unmanned aerial vehicle navigation: without the use of the 399
sitioning system and preloaded maps
fects upon pressure and film thickness in a trochoidal hydrostatic gear
al | aspects of insect-like flapping wings in hover 398
wing design using genetic algorithms and fuzzy logic 145
dynamic analysis for non-linear gas turbine structures 211
sis of aircraft wh}e els using a speckle shearing interferometer 9S
of fitting design 286
stabilization system with |l ow-power magnetic torquers 99-109
thodologies for a thrust reverser cascade using aerodynamic and
yessure and film thickness in a trochoidal hydrostatic
de stabilization system with low-power magnetic torquers 99-109
methodologies for a thrust reverser cascade using aerodynamic and 301-313
rotor — fuselage response using symbolically derived
erivation
coupled rotor — fuselage response using symbolically derived
confirmation and illustrative cases
networks for validation of on-board jet engine data
using genetic algorithms and fuzzy logic
the performance of divided intake ducts
ance of divided intake ducts
id spar load ra on the wing mass for light aircraft
red guidance for application in ground and airborne
for application in ground and airborne
air vehicle: from design concept to research flight
unmanned aerial vehicle navigation: without the use of the 399-416
ind preloaded maps
uircraft wheels using a speckle shearing interferometer 295
aircralt structural monitor ng 329-346
uircraft structures subjected to high-intensity random 242
i coupled rotor — fuselage response using symbolically derived
derivation
of coupled rotor — fuselage response using symbolically derived
Part 2: confirmation and illustratLiIvN e cases
testing
using a new suboptimal control method
thrust reverser cascade using aerodynamic
tion systems for hybrid laminar flow control aircraft
important experimental results
ispects of insect-like flapping wings in hover
inspired guidance for application in ground and airborne
maintenance costs [or