Program developed to support research on National Aero-Space Plane, which takes off horizontally and flies into orbit. SCRAM performs nose-to-tail simulation of real gas flow with equilibrium thermodynamic characteristics encountered in hydrogen-fueled ramjet/scramjet engine. Written for supersonic flows, code modified to handle subsonic flows and dual-mode combustor operation. Written in FORTRAN 77.


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    Title :

    An Engineer's Tool For Prediction Of Airframe Integrated Scramjet Performance (SCRAM)


    Contributors:

    Published in:

    Publication date :

    1990-12-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Scram jet Engine/Airframe Integration Methodology

    Hunt, J. L. / McClinton, C. R. / Advisory Group for Aerospace Research and Development | British Library Conference Proceedings | 1997


    Effects of airframe integrated configuration on scramjet inlet performance

    Akihisa, Daisuke / Masuya, Goro / Kanda, Takeshi et al. | AIAA | 2000


    Effects of Airframe Integrated Configuration on Scramjet Inlet Performance

    Akihisa, D. / Masuya, G. / Kanda, T. et al. | British Library Conference Proceedings | 2000


    Design considerations for the airframe-integrated scramjet

    Henry, J. R. / Anderson, G. Y. | NTRS | 1973


    Design Considerations for the Airframe-Integrated Scramjet

    J. R. Henry / G. Y. Anderson | NTIS | 1973