Effect of Combustor Configuration on Flow and Combustion in a Scramjet Engine

Cited 4 time in webofscience Cited 4 time in scopus
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Publisher
AMER INST AERONAUTICS ASTRONAUTICS
Issue Date
2013-05
Language
English
Article Type
Article
Keywords

SUPERSONIC-COMBUSTION; INLET

Citation

JOURNAL OF PROPULSION AND POWER, v.29, no.3, pp.751 - 756

ISSN
0748-4658
DOI
10.2514/1.B34737
URI
http://hdl.handle.net/10203/174751
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