Numerical analysis on cooling performance of counterflowing jet over aerodisked blunt body
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-014-0517-4.pdf
Reference15 articles.
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3. Mohri, K., Hillier, R.: Computational and experimental study of supersonic flow over axisymmetric cavities. Shock Waves 2, 175–191 (2011)
4. Menezes, V., Saravanan, S., Jagadeesh, G., Reddy, K.P.J.: Experimental investigations of hypersonic flow over highly blunted cones with aero-spikes. AIAA J. 41, 1955–1966 (2003)
5. Gerdroodbary, M.B., Hosseinalipour, S.M.: Numerical simulation of hypersonic flow over highly blunted cones with spike. Acta Astronaut. 67, 180–193 (2010)
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