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


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:

    Publication date :

    1965-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English