Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Effects of Rotating Tabs on Flow and Acoustic Fields of Supersonic Jet


    Author / Creator :

    Mohammed K. Ibrahim, Yoshiaki Nakamura


    Contributors:

    Published in:

    AIAA Journal ; 39 , 4 ; 745-748


    Publication date :

    2001-01-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    The Effects of Vane-Type Tabs on Flow and Acoustic Fields of Supersonic Jet

    Ibrahim, M. K. / Nakamura, Y. / AIAA | British Library Conference Proceedings | 2000


    The effects of vane-type tabs on flow and acoustic fields of supersonic jet

    Ibrahim, Mohammed / Nakamura, Yoshiaki | AIAA | 2000


    Supersonic jet flow control using semi-circular corrugated tabs

    K., Sathish Kumar / Chidambaram, Senthilkumar | Emerald Group Publishing | 2019


    Corrugated Tabs for Supersonic Jet Control

    Phanindra, B. Chiranjeevi / Rathakrishnan, E. | AIAA | 2010