HYDROGEN-FUELED SCRAMJETS: POTENTIAL FOR DETAILED COMBUSTOR ANALYSIS.

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Beach Jr., H.L.
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| 1976年
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V4 [航天（宇宙航行）]; V238 [];
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摘要：
Combustion research related to hypersonic scramjet (supersonic combustion ramjet) propulsion is discussed from the analytical point of view. Because the fuel is gaseous hydrogen, mixing is single-phase and the chemical kinetics are well known. Recent progress in applying two- and three-dimensional analytical techniques to mixing and reacting flows indicates cause for optimism.
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