A model for sonic/supersonic transverse fuel injection into a supersonic airstream is proposed. The model replaces the hydrogen jet up to the Mach disk plane and the elliptic parts of the air flow field around the jet by an equivalent body. The main features of the model were validated on the basis of experimental data.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A model for 3-D sonic/supersonic transverse fuel injection into a supersonic air stream


    Contributors:

    Publication date :

    1989-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    Supersonic transverse injection into a supersonic stream.

    MAHAFFEY, R. E. / SCHETZ, J. A. | AIAA | 1968


    CONTROL OF A TRANSVERSE SUPERSONIC JET INJECTION INTO A SUPERSONIC CROSS-STREAM

    Murugappan, S. / Gutmark, E. / Carter, C. et al. | British Library Conference Proceedings | 2004