Geodesic
Study of temperature field non-uniformity influence on pressure pulsations in inlet duct using RANS/ILES-method
Matematičeskoe modelirovanie, Tome 31 (2019) no. 10, pp. 35-48

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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.
Mots-clés : RANS/ILES, pressure pulsation spectra.
Keywords: supersonic inlet, mixed compression inlet, flow non-uniformity, inlet distortion, buzz 
@article{MM_2019_31_10_a3,
     author = {R. S. Ayupov and L. A. Benderskiy and D. A. Lyubimov},
     title = {Study of temperature field non-uniformity influence on pressure pulsations in inlet duct using {RANS/ILES-method}},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {35--48},
     publisher = {mathdoc},
     volume = {31},
     number = {10},
     year = {2019},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2019_31_10_a3/}
}
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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. Matematičeskoe modelirovanie, Tome 31 (2019) no. 10, pp. 35-48. http://geodesic.mathdoc.fr/item/MM_2019_31_10_a3/