Tatiana A. Kiseleva , Aleksandr D. Kosinov , Yurii G. Ermolaev , Vladislav F. Volkov

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018- 1120

To create a supersonic airplane with low sonic boom, we must develop the physical modeling of this phenomenon. This paper proposes improvement on the experimental method for studies of the airplane near-field. The method based on for simultaneous measurement of pressure and average mass flow rate in the dynamic recording mode in the conditions of the T-313 wind tunnel of the Institute of Theoretical and Applied Mechanics Siberian Branch of the Russian Academy of Sciences. It is shown that the correlation of the average mass flow with the pressure distributions is observed

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In Categories: High-Speed Aerodynamics and Aerothermodynamics, HiSST 2018, Hypersonic Aerodynamics
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