RR–MR transition of a Type V shock interaction in inviscid double-wedge flow with high-temperature gas effects
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/article/10.1007/s00193-017-0770-4/fulltext.html
Reference22 articles.
1. Edney, B.: Anomalous heat transfer and pressure distributions on blunt bodies at hypersonic speeds in the presence of an impinging shock. Technical Report FFA-115, The Aerospace Research Institute of Sweden (1968)
2. Olejniczak, J., Wright, M.J., Candler, G.V.: Numerical study of inviscid shock interactions on double-wedge geometries. J. Fluid Mech. 352, 1–25 (1997). https://doi.org/10.1017/S0022112097007131
3. Lind, C.A., Lewis, M.J.: Unsteady characteristics of a hypersonic type IV shock interaction. J. Aircr. 32, 1286–1293 (1995). https://doi.org/10.2514/3.46876
4. Lind, C.A.: Effect of geometry on the unsteady type-IV shock interaction. J. Aircr. 34, 64–71 (1997). https://doi.org/10.2514/2.2136
5. Ben-Dor, G., Vasilev, E., Elperin, T., Zenovich, A.: Self-induced oscillations in the shock wave flow pattern formed in a stationary supersonic flow over a double wedge. Phys. Fluids 15, L85 (2003). https://doi.org/10.1063/1.1625646
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