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

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

Karanian, A. J. / Kepler, C. E.

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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Title :

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

Contributors:

Karanian, A. J. (author) / Kepler, C. E. (author)

Publication date :

1965-06-01

Type of media :

Conference paper

Type of material :

No indication

Language :

English

Keywords :

SUPERSONIC COMBUSTION RAMJET MISSILE , INLET FLOW , HYPERSONIC INLET , Propulsion Systems , HYDROGEN FUEL

KARANIAN, A. / KEPLER, C. | AIAA | 1965

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