Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Experimental Investigation of Flutter Mechanisms Depending on Sweep Under Subsonic Flow and Low Reynolds Numbers


    Contributors:

    Conference:

    German aerospace aerodynamics and the german society for aeronautics and astronautics (Symposium)



    Publication date :

    2018-01-01


    Size :

    10 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    A Subsonic High-Angle-of-Atiack Flow Investigation at Several Reynolds Numbers

    Mark H. Ciarkson / Gerald N. Malcolm / Gary T. Chapman | AIAA | 1978


    Experimental and Numerical Investigation of Delta Wing Flutter in Low Subsonic Flow

    Hashimoto, A. / Furuta, Y. / Yagi, N. et al. | British Library Conference Proceedings | 2006


    Experimental and Numerical Investigation of Delta Wing Flutter in Low Subsonic Flow

    Hashimoto, Atsushi / Furuta, Yasuyuki / Yagi, Naoto et al. | AIAA | 2006



    Subsonic sphere drag measurements at intermediate Reynolds numbers

    Sivier, Kenneth R. / Nicholls, J. A. | TIBKAT | 1969