1–10 von 31 Ergebnissen
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    ROBUST DESIGN OF AIRCRAFT WING SIZING INCLUDING JIG TWIST SHAPE

    Liu, L. / Scarth, C. / Cooper, J. E. | TIBKAT | 2021

    SIZING OF HIGH ASPECT RATIO WINGS INCORPORATING FOLDING WINGTIP

    Gu, H. / Healy, F. / Cooper, J. E. | TIBKAT | 2021

    Rapid Prediction of Worst-Case Gust Loads Following Structural Modification

    Khodaparast, H. Haddad / Cooper, J. E. | AIAA | 2014

    AIRCRAFT LOADS PREDICTION USING ENHANCED SIMULATION

    Lemmens, Y. / Wilson, T. / Cooper, J. E. | British Library Conference Proceedings | 2018

    Interpretation of Bending/Torsion Coupling for Swept, Nonhomogenous Wings

    Stodieck, O. / Cooper, J. E. / Weaver, P. M. | AIAA | 2015

    Gust and Ground Loads Integration for Aircraft Landing Loads Prediction

    Castrichini, A. / Cooper, J. E. / Benoit, T. et al. | AIAA | 2017

    Enhanced Evolutionary-Based Optimization Techniques Applied to a Nonlinear Landing Gear Design Problem

    Tartaruga, I. / Cooper, J. E. / Lowenberg, M. H. et al. | AIAA | 2019

    Aeroelastic Tailoring of a Representative Wing Box Using Tow-Steered Composites

    Stodieck, O. / Cooper, J. E. / Weaver, P. M. et al. | AIAA | 2016

    Optimization of Tow-Steered Composite Wing Laminates for Aeroelastic Tailoring

    Stodieck, O. / Cooper, J. E. / Weaver, P. M. et al. | AIAA | 2015

    Testing of Folding Wingtip for Gust Load Alleviation of Flexible High-Aspect-Ratio Wing

    Cheung, R. C. M. / Rezgui, D. / Cooper, J. E. et al. | AIAA | 2020