An experimental and computational investigation of hypervelocity, hypersonic combustion of hydrogen with air is described which was intended to confirm the presence of combustion at these conditions and then to gauge the pressure rise associated with the heat release of combustion. Experiments were conducted in a square cross section duct and wall pressure was measured. It was found that combustion did occur and that the maximum pressure increase was approximately 72 percent over the intake pressure.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hydrogen combustion in a hypersonic airstream


    Beteiligte:
    Casey, R. T. (Autor:in) / Stalker, R. J. (Autor:in) / Brescianini, C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.05.1992



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch