Supersonic combustion ramjet engine, `scramjet,' for powering both hypersonic aircraft and satellite boosting is theoretically superior to present rocket engine; tailored interface hypersonic shock tunnel provides means by which conditions in combustion chamber can be simulated for short periods of time; for maximum testing times, tailored operation of tunnel is essential.


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    Title :

    Shock tunnel as supersonic combustion test facility


    Additional title:

    Fuel Soc J


    Contributors:
    Wood, M.P. (author)

    Published in:

    Publication date :

    1966


    Size :

    11 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English