Flow parameters in chart form and calculated for air as real gas in chemical equilibrium for series of stagnation temperatures between 2790 and 4950 R and pressures up to 1000 atm; from these charts it is possible to calibrate hypersonic nozzle in conventional way; method for calculating inviscid nozzle contour including real-gas effects.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Erickson, W.D. (Autor:in) / Creekmore, H.S. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    179 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :