Research status of key techniques for shock-induced combustion ramjet (shcramjet) engine
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-009-0379-7.pdf
Reference24 articles.
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2. Couture D, Dechamplain A, Stowe R A, et al. Comparison of scramjet and shcramjet propulsion for a hypersonic waverider configuration. AIAA Paper 2008-5171, 2008
3. Wang Y W, Sislian J P. Numerical investigation of methane and air mixing in a shcramjet inlet. AIAA Paper 2008-2533, 2008
4. Dudebout R, Sislian J P, Oppitz R. Numerical simulation of hypersonic shock-induced combustion ramjets. J Propul Power, 1998, 14(6): 869–879
5. Schwartzentruber T E, Sislian J P, Parent B. Suppression of premature ignition in the premixed inlet flow of a shcramjet. J Propul Power, 2005, 21(1): 87–94
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