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    Title :

    Convolution Kernels for a NACA 0012 Airfoil Based on Unsteady Pressure Wind Tunnel Measurements


    Contributors:

    Conference:

    AIAA SCITECH 2024 Forum



    Publication date :

    2024-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Heat transfer measurements from a smooth NACA 0012 airfoil

    POINSATTE, PHILIP E. / VAN FOSSEN / G. J. et al. | AIAA | 1991


    Investigation of NACA 0012 Airfoil Periodic Flows in a Transonic Wind Tunnel

    Ren, X. / Zhao, Z. / Gao, C. et al. | British Library Conference Proceedings | 2013


    Investigation of NACA 0012 Airfoil Periodic Flows in a Transonic Wind Tunnel

    Ren, Xudong / Zhao, Zijie / Gao, C. et al. | AIAA | 2013


    Heat transfer measurements from a smooth NACA 0012 airfoil

    Poinsatte, Philip E. / Van Fossen, G. J. / Newton, James E. et al. | NTRS | 1991


    Numerical Simulation of a Pitching NACA 0012 Airfoil

    Pechloff, A. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2000