| Introduction to aircraft aeroelasticity and loads JR Wright, JE Cooper John Wiley & Sons, 2008 | 1209 | 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 | 334 | 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 | 237 | 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 | 209 | 2001 |
| 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 | 190 | 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 | 190 | 1998 |
| Identification of backbone curves of nonlinear systems from resonance decay responses JM Londoño, SA Neild, JE Cooper Journal of Sound and Vibration 348, 224-238, 2015 | 179 | 2015 |
| Improved aeroelastic tailoring using tow-steered composites O Stodieck, JE Cooper, PM Weaver, P Kealy Composite Structures 106, 703-715, 2013 | 177 | 2013 |
| Design and development of aircraft systems I Moir, A Seabridge, P Belobaba, J Cooper John Wiley & Sons, 2012 | 157 | 2012 |
| 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 | 142 | 2016 |
| 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 | 129 | 2017 |
| 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 | 124 | 2007 |
| 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 | 118 | 2017 |
| Flutter prediction from flight flutter test data G Dimitriadis, JE Cooper Journal of Aircraft 38 (2), 355-367, 2001 | 107 | 2001 |
| Hopf bifurcation analysis of a rotor/seal system Q Ding, JE Cooper, AYT Leung Journal of Sound and Vibration 252 (5), 817-833, 2002 | 106 | 2002 |
| 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 | 98 | 2014 |
| 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 | 91 | 2001 |
| Normal-mode force appropriation—theory and application JR Wright, JE Cooper, MJ Desforges Mechanical Systems and Signal Processing 13 (2), 217-240, 1999 | 89 | 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 | 86 | 2015 |
| Design of composite wings including uncertainties: a probabilistic approach A Manan, J Cooper Journal of Aircraft 46 (2), 601-607, 2009 | 83 | 2009 |
