It is assumed that flow is unidimensional; specific heats of gas are same before and after combustion; flow is adiabatic before combustion and that in sections of air inlet where there are no shock waves flow is isentropic; three main methods of measuring thrust; strain-gage method, thermodynamic method and aerodynamic method; charts giving results obtained in actual flight. In French with English translation of principal parts.


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    Titel :

    Flight measurements of ramjet and rocket thrust


    Weitere Titelangaben:

    Stato-reacteur ef fusee -- Determination de la poussee en vol


    Beteiligte:
    Bourgarel, C. (Autor:in) / Beslon, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1958


    Format / Umfang :

    29 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Französisch





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