1–18 von 18 Ergebnissen
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    Drag Reduction by Boundary-Layer Combustion: Influence from Disturbances Typical of Cross-Stream Fuel-Injection

    Chan, Wilson Y. K. / Mee, David J. / Smart, Michael K. et al. | AIAA | 2015

    Freejet Testing of the HIFiRE 7 Scramjet Flowpath at Mach 7.5

    Chan, Wilson Y. K. / Razzaqi, Sarah A. / Turner, James C. et al. | AIAA | 2018

    Unsteady transonic flows with shock waves in an asymmetric channel

    CHAN, J. S.-K. / ADAMSON, T. C. | AIAA | 1978

    Ignition Experiments of Hydrocarbons in a Mach 8 Shape-Transitioning Scramjet Engine

    Denman, Zachary J. / Chan, Wilson Y. K. / Brieschenk, Stefan et al. | AIAA | 2016

    Hybrid optimisation strategy beyond local optima in aerospace panel designs

    Chan, K. / Kennedy, D. / Williams, F. | AIAA | 1998

    Asymptotic Solution for Nonlinear Buckling of Orthotropic Shells on Elastic Foundation

    Nie, G. H. / Chan, C. K. / Yao, J. C. et al. | AIAA | 2009

    Hybrid Optimization Strategy Beyond Local Optima in Aerospace Panel Designs

    K. Leung Chan / David Kennedy / Fred W. Williams | AIAA | 1999

    Aerodynamic Design of Nozzles with Uniform Outflow for Hypervelocity Ground-Test Facilities

    Chan, Wilson Y. K. / Jacobs, Peter A. / Smart, Michael K. et al. | AIAA | 2018

    Preliminary Evaluation of the SAFE-Cue Warning Display for Loss of Control Mitigation

    Lampton, Amanda K. / Klyde, David H. / Lee, Dong-Chan et al. | AIAA | 2015

    Yaw and Angle of Attack Measurements on the NASA CV-990 Aircraft

    BOWEN, STUART / SCOTT, STANLEY / CHAN, K. et al. | AIAA | 1985