1–20 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

    Nonlinear Negative Stiffness Wingtip Spring Device for Gust Loads Alleviation

    Castrichini, A. / Cooper, J. E. / Wilson, T. et al. | AIAA | 2016

    Uncertainty and Sensitivity Analysis of Bifurcation Loci Characterizing Nonlinear Landing-Gear Dynamics

    Tartaruga, I. / Cooper, J. E. / Lowenberg, M. H. et al. | AIAA | 2017

    Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device

    Castrichini, A. / Wilson, T. / Saltari, F. et al. | AIAA | 2019

    AEROELASTICS FLIGHT DYNAMICS COUPLING EFFECTS OF THE SEMI AEROELASTIC HINGE DEVICE - IFASD 2019

    Castrichini, A. / Saltari, F. / Viceconti, N. et al. | TIBKAT | 2020

    Slender-Wing Beam Reduction Method for Gradient-Based Aeroelastic Design Optimization

    Stodieck, O. / Cooper, J. E. / Neild, S. A. et al. | AIAA | 2018

    Prediction and uncertainty propagation of correlated time-varying quantities using surrogate models

    Tartaruga, I. / Cooper, J. E. / Lowenberg, M. H. et al. | Springer Verlag | 2015

      Prediction and uncertainty propagation of correlated time-varying quantities using surrogate models

      Tartaruga, I. / Cooper, J. E. / Lowenberg, M. H. et al. | Online Contents | 2015

    Earth Radiation budget satellite system studies

    Woerner, C. V. / Cooper, J. E. | NTRS | 1977

    System implementation for Earth Radiation Budget Satellite System

    Cooper, J. E. / Woerner, C. V. | NTRS | 1978

    Force Appropriation for Flight Flutter Testing

    Desforges, M. J. / Cooper, J. E. / Wright, J. R. | British Library Conference Proceedings | 1995

    Sizing High-Aspect-Ratio Wings with a Geometrically Nonlinear Beam Model

    Calderon, D. E. / Cooper, J. E. / Lowenberg, M. et al. | AIAA | 2019