Numerical studies on the mixing of CH4 and kerosene injected into a supersonic flow with H2 pilot injection
Author:
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/content/pdf/10.1007/BF02438312.pdf
Reference13 articles.
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2. Waltrup P J. Liquid fueled supersonic combustion ramjets. A research prospective of the past, present and future[A]. AIAA Paper. 86-0158, 1986.
3. Andrews E H, Trexler C A, Emami S. Tests of a fixed-geometry inlet-combustor configuration hydrocarbon-fueled, dual-mode scramjet[A]. AIAA Paper, 94-2817, 1994.
4. Billig F S. Supersonic combustion ramjet technology missile[J].J Propulsion and Power, 1995,11(1): 1139–1146.
5. Narayanan A K, Damadaran K A. Experimental studies on piloted supersonic combustion using the petal nozzle[J].J Propulsion and Power, 1997,13(1):142–148.
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