1–20 von 28 Ergebnissen
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    Enhancing MAV Stability in Gusty Wind by Wing Flexibility - Analyses and Flight Tests

    Kuo, C.-M. / Boller, C. / Qin, N. | British Library Conference Proceedings | 2007

    Using the Medial Axis to Represent Complex Flow Structures for Flow Feature-Aligned Mesh Generation

    Harris, M. / Qin, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    COMPARISON OF RANS, DES AND DDES RESULTS FOR ONERA M-6 WING AT TRANSONIC FLOW SPEED USING AN IN-HOUSE PARALLEL CODE

    Durrani, N. / Qin, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    METAMODELS FOR AEROTHERMODYNAMIC DESIGN OPTIMIZATION OF HYPERSONIC SPIKED BLUNT BODIES

    Ahmed, M. / Qin, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010

    Fluid-Structure Interaction of HALE Wing Configuration with an Efficient Moving Grid Method

    Carnie, G. / 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

    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

    THREE DIMENSIONAL ADAPTIVE METHOD FOR COMPRESSIBLE MULTI-FLUIDS FLOWS

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

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

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

    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

    A MUSCL AND WENO - PNS APPROACH FOR VORTEX DOMINATED FLOWFIELDS

    de Feo, D. / Qin, N. / Birch, T. et al. | British Library Conference Proceedings | 2010

    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

    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

    Effects of Compressibility and Roughness for Turbulence Modelling of Hypersonic Ramp Flow

    Richardson, G. / Qin, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1999

    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

    BILU Implicit Multiblock Euler/Navier-Stokes Simulation for Helicopter Rotor Vortical Flow

    Zhong, B. / Shaw, S. T. / Qin, N. et al. | British Library Conference Proceedings | 2005

    ADAPTIVE WING/AEROFOIL DESIGN OPTIMISATION USING MOEA COUPLED TO UNCERTAINTY DESIGN METHOD

    Lee, D. / Periaux, J. / Gonzalez, L. et al. | British Library Conference Proceedings | 2011