Yang, V. and Culick, F. E. C. (1984) Numerical calculations of pressure oscillations in a side-dump ramjet engine. AIAA Papers, AIAA-1984-365 . American Institute of Aeronautics and Astronautics . http://resolver.caltech.edu/CaltechAUTHORS:20101209-115108188
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Pressure oscillations in a side-dump ramjet engine have been studied, using a one-dimensional numerical analysis. The engine is treated in two parts; the inlet section, including a region of two-phase flow downstream of fuel injection, and a dump combustor. Each region is treated separately and matched with the other. Following calculation of the mean flow field, the oscillatory characteristics of the engine are determined by its reponse to a disturbance imposed on the mean fiow. Results have shown favorable comparison with experimental data obtained at the Naval Weapons Center, China Lake.
|Item Type:||Report or Paper (Report)|
|Additional Information:||© 1984 AIAA. The authors are indebted to Mr. J. N. Levine for providing the current numerical code for the self adjusting hybrid scheme, and to W. H. Clark and J. W. Humphrey for several informative conversations. This work represents a part of the results obtained from the research program supported partly by the California Institute of Technology and partly by the Air Force Office of Scientific Research, Grant No. AFOSR-80-0265.|
|Group:||Guggenheim Jet Propulsion Center, GALCIT|
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|Official Citation:||Numerical calculations of pressure oscillations in a side-dump ramjet engine CULICK, F.E.C., California Institute of Technology, Pasadena, CA AIAA-1984-365 American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting, 22nd, Reno, NV, Jan 9-12, 1984. 9 p|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Ruth Sustaita|
|Deposited On:||15 Dec 2010 18:10|
|Last Modified:||22 Sep 2016 21:52|
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