Experimental study of the impact of N-wave on heat transfer in a boundary layer of a flat plate at the Mach number 2
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Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0051930
Reference14 articles.
1. S. A. Gaponov and A. A. Maslov, Development of Disturbances in Compressible Flows (Nauka, Novosibirsk 1980). [in Russian].
2. V. A. Lebiga, A. A. Maslov, and V. G. Pridanov, Archives Mech. 31(3), 397–405 (1979).
3. Aerodynamic Noise in Supersonic Wind Tunnels
4. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition
5. Numerical Modeling of the Interaction between a Supersonic Boundary Layer and an Acoustic Wave
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