41–60 von 83 Ergebnissen
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    Numerical Simulation of Flexible Flapping Airfoil Propulsion using Dynamic Mesh at Low Reymolds Numbers

    Durrani, N. / Qin, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    Adjoint Based Aerodynamic Optimisation of a UCAV

    Coppin, J. / Qin, N. / Birch, T. et al. | British Library Conference Proceedings | 2013

    Aerodynamic considerations of blended wing body aircraft

    Qin, N. / Vavalle, A. / Le Moigne, A. et al. | Elsevier | 2004

    THREE DIMENSIONAL ADAPTIVE METHOD FOR COMPRESSIBLE MULTI-FLUIDS FLOWS

    Zheng, H. / Qin, N. / Shu, C. et al. | British Library Conference Proceedings | 2010

    Calculation of pitch damping coefficients for projectiles

    Qin, N. / Ludlow, D. / Shaw, S. et al. | AIAA | 1997

      Calculation of Pitch Damping Coefficients for Projectiles

      Qin, N. / Ludlow, D. K. / Shaw, S. T. et al. | British Library Conference Proceedings | 1997

    AIAA-2002-5448 Aerodynamic Studies for Blended Wing Body Aircraft

    Qin, N. / American Institute of Aeronautics and Astronautics / ISSMO | British Library Conference Proceedings | 2002

    Intuitive Class/Shape Function Parameterization for Airfoils

    Zhu, F | Online Contents | 2014
    Beteiligte: Qin, N

    AIAA 2006-1258 LES with Numerical Dissipation for Aircraft Wake Vortices

    Le Moigne, A. / Qin, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006

    The influence of transition onset location on the performance of shock control bumps

    McIntosh, S C | Online Contents | 2013
    Beteiligte: Qin, N

    Behavior of Detached-Eddy Simulations for Mild Airfoil Trailing-Edge Separation

    Durrani, N | Online Contents | 2011
    Beteiligte: Qin, N

    2-D NUMERICAL ANALYSIS OF A VAWT WIND FARM FOR DIFFERENT CONFIGURATIONS

    Durrani, N. / Qin, N. / Hameed, H. et al. | British Library Conference Proceedings | 2011

    Drag Reduction Using Aerodisks for Hypersonic Hemispherical Bodies

    Ahmed, M Y M | Online Contents | 2010
    Beteiligte: Qin, N

    Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps AIAA Paper

    Qin, N. / Wong, S. / Le Moigne, A. et al. | British Library Conference Proceedings | 2007

    Numerical Prediction of the Aerodynamic Response of Aerofoils Subjected to Step Increase in Mach Number

    Shaw, S. / Qin, N. / Deutsche Gesellschaft fur Luft und Raumfahrt | British Library Conference Proceedings | 1997

    Wind Tunnel and Numerical Study of a Small Vertical Axis Wind Turbine

    Edwards, J. / Durrani, N. / Howell, R. et al. | British Library Conference Proceedings | 2008

    Iterative Response Surface Based Optimization Scheme for Transonic Airfoil Design

    Vavalle, A. | Online Contents | 2007
    Beteiligte: Qin, N.