Recent analyses showed advantages of supersonic combustion for hypersonic ramjet; experiment in shock-induced combustion was undertaken to show relation between experimental results and kinetic calculations, and to interpret results in terms of possible use of phenomenon for hypersonic air-breathing propulsion; it is concluded that detonations are special case of shock induced combustion; quenched gaseous components for early parts of chemical reaction were analyzed to determine hydrogen molecule reaction rate, and comparison was made of experimental H2 reaction rate, with current chemical kinetic computations.


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    Title :

    Shock-induced combustion with oblique shocks -- Comparison of experiment and kinetic calculations


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 1 , n 12


    Publication date :

    1963


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English







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