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JOURNALS // Matematicheskoe modelirovanie // Archive

Mat. Model., 2019 Volume 31, Number 10, Pages 35–48 (Mi mm4116)

This article is cited in 3 papers

Study of temperature field non-uniformity influence on pressure pulsations in inlet duct using RANS/ILES-method

R. S. Ayupov, L. A. Benderskiy, D. A. Lyubimov

Central Institute of Aviation Motors

Abstract: The paper is dedicated to application of high resolution RANS/ILES-method for study of temperature field non-uniformity influence on throttle characteristic, sound pressure level and pressure pulsation spectra of supersonic mixed compression inlet. Five cases of inflow were investigated, three of them were non-uniform. Sound pressure level distribution in the inlet duct and pressure pulsation spectra on inlet walls were obtained.

Keywords: RANS/ILES, supersonic inlet, mixed compression inlet, flow non-uniformity, inlet distortion, buzz, pressure pulsation spectra.

Received: 04.03.2019
Revised: 04.03.2019
Accepted: 08.04.2019

DOI: 10.1134/S0234087919100034


 English version:
Mathematical Models and Computer Simulations, 2020, 12:3, 378–387

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© Steklov Math. Inst. of RAS, 2025