Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Numerical Flowfield Visualization over Heat Shield of Satellite Launch Vehicle at Mach 0.8 - 3.0


    Contributors:
    Mehta, R C (author)

    Published in:

    Publication date :

    2011



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.50 / 55.60



    Multi-body launch vehicle flowfield simulation

    WANG, J. / THAN, P. / WIDHOPF, G. | AIAA | 1991


    Shockwave Oscillations Over the Conical Heat Shield Region of a Typical Launch Vehicle at Mach 0.95

    Murugan, K. N. / Arunkumar, T. / Prasath, M. et al. | TIBKAT | 2021


    Shockwave Oscillations Over the Conical Heat Shield Region of a Typical Launch Vehicle at Mach 0.95

    Murugan, K. N. / Arunkumar, T. / Prasath, M. et al. | Springer Verlag | 2021