Hypersonic inlet performance estimates used to predict thrust and fuel specific impulse possible with hydrogen fueled subsonic and supersonic combustion ramjets


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    Titel :

    Experimental hypersonic inlet investigation with application to dual-mode scramjet.


    Beteiligte:
    Karanian, A. J. (Autor:in) / Kepler, C. E. (Autor:in)

    Erscheinungsdatum :

    1965-06-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





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