Shock wave configurations and flow structures in non-axisymmetric underexpanded sonic jets
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-010-0257-z.pdf
Reference18 articles.
1. Addy A.L.: Effects of axisymmetric sonic nozzle geometry on Mach disk characteristics. AIAA J. 19, 121–122 (1981)
2. Alkislar M.B., Krothapalli A., Lourenco L.M.: Structure of a screeching rectangular jet: a stereoscopic particle image velocimetry study. J. Fluid Mech. 489, 121–154 (2003)
3. Courant R., Friedrichs K.O.: Supersonic flow and shock waves. Interscience, New York (1956)
4. Gutmark E., Schadow K.C., Bicker C.J.: Near acoustic field and shock structure of rectangular supersonic jets. AIAA J. 28, 1163–1170 (1990)
5. Loh, C.Y., Himansu, A., Wang, X.Y., Jorgenson, P.C.E.: Computation of an underexpanded 3-d rectangular jet by the CE/SE method. Technical Report NASA TM 2000-210594 (2000)
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