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Interaction of long-wave perturbations with a shock wave on a wedge and method of mode decomposition of supersonic flow pulsationsJournal of Physics: Conference Series, 894
I. Tsyryulnikov, A. Maslov, S. Mironov, T. Poplavskaya, S. Kirilovskiy (2015)
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Evolution of disturbances in the shock layer on a flat plate in the flow of a mixture of vibrationally excited gasesThermophysics and Aeromechanics, 24
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Coefficients of transformation of long-wavelength perturbations of a supersonic incident flow around a wedge into pressure fluctuations on its surfaceTechnical Physics Letters, 42
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Controlled disturbances are inserted into the wind tunnel flow, and probing measurements of the fields of the amplitudes of pressure and phase velocity oscillations of these disturbances are performed. Based on the relations for inviscid interaction of long-wave vortex, entropy, and acoustic disturbances with the shock wave on a wedge and numerical simulations, the coefficients of conversion of various modes to pressure oscillations on the model surface are determined for the test conditions of a supersonic flow in the T-327B blowdown wind tunnel located at the Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences. The method of mode decomposition for controlled disturbances with the use of disturbance conversion coefficients is implemented in the case of a flat plate model with a sharp leading edge aligned at different angles of attack and side-slip in the flow.
Thermophysics and Aeromechanics – Springer Journals
Published: Feb 20, 2021
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