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This article is cited in 3 scientific papers (total 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
Citation:
R. S. Ayupov, L. A. Benderskiy, D. A. Lyubimov, “Study of temperature field non-uniformity influence on pressure pulsations in inlet duct using RANS/ILES-method”, Mat. Model., 31:10 (2019), 35–48; Math. Models Comput. Simul., 12:3 (2020), 378–387
Linking options:
https://www.mathnet.ru/eng/mm4116 https://www.mathnet.ru/eng/mm/v31/i10/p35
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