The development of simulation codes for hypersonic flow computations is the pacing item in the definition of a reentry vehicule such as the European HERMES, in order to complement the experimental facilities which cannot cover the complete flight envelope. An important step is the validation of the codes with wind tunnel data and flight test results. Some validations are presented in this paper indicating that the models of the physical and chemical phenomena are satisfactory.


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    Title :

    Some validations by experimental results in hypersonic flow computations


    Additional title:

    Einige experimentelle Beweise fuer die Gueltigkeit von Ueberschallstroemungsberechnungen


    Contributors:
    Bez, J.P. (author) / Chattot, J.J. (author) / Noel, F. (author)

    Published in:

    SAE-Papers ; Apr ; 1-16


    Publication date :

    1988


    Size :

    16 Seiten, 12 Bilder, 7 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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