Characteristics of Shock Train Flow in Divergent Channels
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Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-15-1892-8_28
Reference20 articles.
1. Delery JM (1985) Shock wave/turbulent boundary layer interaction and its control. Prog Aerospace Sci 22(4):209–280
2. Neumann EP, Lustwerk F (1949) Supersonic diffusers for wind tunnels. J Appl Mech 16(2):195–202
3. Newman EP, Lustwerk F (1951) High-effciency supersonic diffusers. J Aeronaut Sci 18(6):369–374
4. Shapiro AH (1953) The dynamics and thermodynamics of compressible Fluid Flow, vols 1 and 2. Ronald Press New York, 135–139, 1153–1156
5. Matsuo Kazuyasu, Miyazato Yoshiaki, Kim Heuy-Dong (1999) Shock train and pseudo-shock phenomena in internal gas flows. Prog Aerosp Sci 35:33–100
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