Zobrazeno 1 - 10
of 28
pro vyhledávání: '"M. Yu. Zaytsev"'
Publikováno v:
Acoustical Physics. 69:182-192
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e0b1699ad7ee6eabf1fd3a2c0fbcce46
https://doi.org/10.1134/s1063771023700562
https://doi.org/10.1134/s1063771023700562
Publikováno v:
Acoustical Physics. 69:252-258
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::236420915ea7814bf1bdb708a8fa36b2
https://doi.org/10.1134/s1063771023600067
https://doi.org/10.1134/s1063771023600067
Publikováno v:
Doklady Physics. 67:328-334
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::98762c1a9852379d45d380d7db7f187d
https://doi.org/10.1134/s1028335822090038
https://doi.org/10.1134/s1028335822090038
Publikováno v:
Doklady Physics. 67:315-327
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cb5af6380540bdc3a369f8177ffe6627
https://doi.org/10.1134/s1028335822090099
https://doi.org/10.1134/s1028335822090099
Publikováno v:
Acoustical Physics. 65:297-306
An experimental study of noise reduction methods has been carried out for realistic small-scale (1 : 10) models of aircraft landing gear based on two ideas: (1) the useful interference of turbulent wake sources and reflected sources induced by them,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::57231bcfd52a355755375773e2dcd6e7
https://doi.org/10.1134/s1063771019030011
https://doi.org/10.1134/s1063771019030011
Autor:
Evgeniya Cherenkova, Vadim Palchikovskiy, Victor Kopiev, I. V. Khramtsov, O. Yu. Kustov, M. Yu. Zaytsev
Publikováno v:
Acoustical Physics. 64:503-510
A technique for studying the aeroacoustic parameters of vortex rings with various diameters in an anechoic chamber is developed. The motion trajectories of vortex rings produced by a piston generator with nozzles with various exit diameters are studi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::85c6f350a14e0da517eed028cf466ee9
https://doi.org/10.1134/s1063771018040097
https://doi.org/10.1134/s1063771018040097
Publikováno v:
Journal of Physics: Conference Series. 2127:012009
A study of the instantaneous and average velocity and vorticity fields in the flow created by the model helicopter rotor in the hover mode was carried out. The velocity fields of the flow generated by the model rotor were obtained by a two-dimensiona
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ac7347402919d1f54fc175eee9244dc4
https://doi.org/10.1088/1742-6596/2127/1/012009
https://doi.org/10.1088/1742-6596/2127/1/012009
Publikováno v:
Acoustical Physics. 63:686-698
The aeroacoustic characteristics of a helicopter rotor are calculated by a new method, to assess its applicability in assessing rotor performance in hovering. Direct solution of the Euler equations in a noninertial coordinate system is used to calcul
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8d625c9a32bba9ea07999567c2460663
https://doi.org/10.1134/s1063771017060070
https://doi.org/10.1134/s1063771017060070
Publikováno v:
Acoustical Physics. 63:14-25
Jet–flap interaction noise for a small-scale swept wing model of a trendsetter plane has been studied experimentally, with a double-stream nozzle installed nearby. The effect of the flap angle on the noise of jet–wing interaction has been analyze
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9d608b2ef211b427b8c62d0f8d2bbdb
https://doi.org/10.1134/s1063771016060026
https://doi.org/10.1134/s1063771016060026
Publikováno v:
Acoustical Physics. 62:97-107
The acoustic characteristics of a large-scale model of a wing with high-lift devices in the landing configuration have been studied in the DNW-NWB wind tunnel with an anechoic test section. For the first time in domestic practice, data on airframe no
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::907172e1e79220a7587bff906cc49327
https://doi.org/10.1134/s1063771015060068
https://doi.org/10.1134/s1063771015060068