Jonathan Cooper
Jonathan Cooper
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Introduction to aircraft aeroelasticity and loads
JR Wright, JE Cooper
John Wiley & Sons, 2008
An eigensystem realisation algorithm using data correlations (ERA/DC) for modal parameter identification
JN Juang, JE Cooper, J Wright
Control-theory and advanced technology 4 (1), 5-14, 1988
Blade-tip timing measurement of synchronous vibrations of rotating bladed assemblies
G Dimitriadis, IB Carrington, JR Wright, JE Cooper
Mechanical Systems and Signal Processing 16 (4), 599-622, 2002
A combined modal/finite element analysis technique for the dynamic response of a non-linear beam to harmonic excitation
MI McEwan, JR Wright, JE Cooper, AYT Leung
Journal of Sound and Vibration 243 (4), 601-624, 2001
Applications of probability density estimation to the detection of abnormal conditions in engineering
MJ Desforges, PJ Jacob, JE Cooper
Proceedings of the institution of mechanical engineers, part c: Journal of …, 1998
A comparison of blade tip timing data analysis methods
IB Carrington, JR Wright, JE Cooper, G Dimitriadis
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2001
Identification of backbone curves of nonlinear systems from resonance decay responses
JM Londoņo, SA Neild, JE Cooper
Journal of Sound and Vibration 348, 224-238, 2015
Improved aeroelastic tailoring using tow-steered composites
O Stodieck, JE Cooper, PM Weaver, P Kealy
Composite Structures 106, 703-715, 2013
Nonlinear folding wing tips for gust loads alleviation
A Castrichini, V Hodigere Siddaramaiah, DE Calderon, JE Cooper, ...
Journal of Aircraft 53 (5), 1391-1399, 2016
Non-linear aeroelastic prediction for aircraft applications
MJC Henshaw, KJ Badcock, GA Vio, CB Allen, J Chamberlain, I Kaynes, ...
Progress in Aerospace Sciences 43 (4-6), 65-137, 2007
Hopf bifurcation analysis of a rotor/seal system
Q Ding, JE Cooper, AYT Leung
Journal of Sound and Vibration 252 (5), 817-833, 2002
Aeroelastic tailoring of a representative wing box using tow-steered composites
O Stodieck, JE Cooper, PM Weaver, P Kealy
AIAA journal 55 (4), 1425-1439, 2017
Flutter prediction from flight flutter test data
G Dimitriadis, JE Cooper
Journal of Aircraft 38 (2), 355-367, 2001
Preliminary investigation of use of flexible folding wing tips for static and dynamic load alleviation
A Castrichini, VH Siddaramaiah, DE Calderon, JE Cooper, T Wilson, ...
The Aeronautical Journal 121 (1235), 73-94, 2017
Uncertainty quantification of aeroelastic stability of composite plate wings using lamination parameters
C Scarth, JE Cooper, PM Weaver, GHC Silva
Composite Structures 116, 84-93, 2014
Normal-mode force appropriation—theory and application
JR Wright, JE Cooper, MJ Desforges
Mechanical Systems and Signal Processing 13 (2), 217-240, 1999
Optimization of tow-steered composite wing laminates for aeroelastic tailoring
O Stodieck, JE Cooper, PM Weaver, P Kealy
AIAA Journal 53 (8), 2203-2215, 2015
A finite element/modal technique for nonlinear plate and stiffened panel response prediction
M McEwan, J Wright, J Cooper, A Leung
19th AIAA Applied Aerodynamics Conference, 1595, 2001
Structural optimization of dental restorations using the principle of adaptive growth
G Couegnat, SL Fok, JE Cooper, AJE Qualtrough
Dental Materials 22 (1), 3-12, 2006
Dynamic multivariate statistical process control using subspace identification
RJ Treasure, U Kruger, JE Cooper
Journal of Process Control 14 (3), 279-292, 2004
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