A. KARANIAN, C. Edward Kepler
Abstract
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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Hypersonic inlet performance estimates used to predict thrust and fuel specific impulse possible with hydrogen fueled subsonic and supersonic combustion ramjets
Key concepts: Scramjet, Hypersonic speed, Dual (grammatical number), Dual mode, Aerospace engineering, Inlet, Mode (computer interface), Materials science