Experimental study of the relationship between the pulsations of the oncoming flow and the disturbances of the boundary layer of a sharp plate at Mach number M=2.5
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Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0132410
Reference8 articles.
1. About the Relationship between Disturbances in a Free Supersonic Flow and Disturbances in a Boundary Layer at Mach Number 2
2. Cross-correlation measurement of disturbance initiated by weak shock wave in the flat plate boundary layer with blunt leading edge at Mach 2
3. L. V. Afanasev, A. D. Kosinov, A. A. Yatskikh, V. L. Kocharin, N. V. Semionov, and Y. G. Yermolaev, “Measurement of the correlation of disturbances from a weak shock wave and pulsations of the boundary layer of a flat plate with a blunted leading edge at Mach 2,” in International Conference on The Methods of Aerophysical Research, Abstracts, edited by A.N. Shiplyuk (Parallel, Novosibirsk, 2020).
4. V. L. Kocharin, A. D. Kosinov, A. A. Yatskikh, L. V. Afanasev, Yu. G. Ermolaev, and N. V. Semionov, J. Phys.: Conf. Ser. 1404, 012083 (2019).
5. Experimental investigation of effect of an external wave on supersonic boundary layer of the blunt flat plate
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