Asymmetry of a Flow Which is Due to the Interaction of a Compression Shock with the Boundary Layer on a Longitudinally Ribbed Surface

Author:

Mazhul’ I. I.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,Condensed Matter Physics

Reference18 articles.

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3. F. Falempa, M. A. Gol′dfel′d, Yu. V. Semenova, A. V. Starov, and K. Yu. Timofeev, Experimental investigation of different methods for control of a hypersonic air intake, Teplofiz. Aéromekh., 15, No. 1, 1–10 (2008).

4. M. A. Gol′dfel′d, Influence of the velocity of the flow over the compression surfaces of an air intake on the efficiency of removal of the boundary layer, Sib. Fiz. Zh., 14, No. 3, 15–25 (2019).

5. Yu. P. Gounko, I. I. Mazhul, and A. M. Kharitonov, Aerodynamic design and experimental modeling of an innovative supersonic three-dimensional air-intake, Aeronaut. J., 117, No. 1192, 559–584 (2013).

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