Výsledky vyhledávání - "I. V. Struminskaya"

Entropy-Layer Influence on Single-Fin and Double-Fin/Boundary-Layer Interactions

Autor: Vladimir Nikolaevich Radchenko, I. V. Struminskaya, Vladimir Evguenyevich Mosharov, A. S. Skuratov, Ivan Vladimirovich Egorov, Volf Ya. Borovoy

Publikováno v: AIAA Journal. 54:443-457

The influence of the entropy layer generated by the blunted-plate leading edge on the flow over a single fin or pair of fins installed on the plate is studied experimentally and numerically. Experiments are carried out in a Ludwieg-type wind tunnel a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::2f00c8c26407f33e967226c756d01b91
https://doi.org/10.2514/1.j053656

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Leading edge bluntness effect on the flow in a model air-inlet

Autor: A. S. Skuratov, Vladimir Nikolaevich Radchenko, Vladimir Evguenyevich Mosharov, I. V. Struminskaya, V. Ya. Borovoy

Publikováno v: Fluid Dynamics. 49:454-467

Flow in an idealized air-inlet with plane walls and a rectangular cross-section is experimentally investigated. The air-inlet is mounted on a plate, at a distance well removed from its leading edge. The experiments were conducted in a Ludwig tube at

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::7d919576fd871c7c08f872ca950a775e
https://doi.org/10.1134/s0015462814040061

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Interaction of intersecting shocks with a flat-plate boundary layer in the presence of an entropy layer

Autor: Ivan Vladimirovich Egorov, Vladimir Nikolaevich Radchenko, A. S. Skuratov, I. V. Struminskaya, Vladimir Evguenyevich Mosharov, V. Ya. Borovoy

Publikováno v: Fluid Dynamics. 48:636-647

Gas flow and heat transfer on the surfaces of sharp and blunt plates is experimentally investigated in the presence of two forward-looking wedges at the Mach numbers M = 5, 6, and 8 and the Reynolds numbers up to Re∞L = 27×106. It is shown that th

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::9b7638215e253399c327177148a7cfe7
https://doi.org/10.1134/s0015462813050074

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Starting of generic inlet with blunted wedges

Autor: V. Borovoy, V. Radchenko, I. V. Struminskaya, V. Mosharov, A. Skuratov

Publikováno v: Progress in Flight Physics.

Bluntness e¨ect of gas-compressing wedges on starting and §ow structure in an air inlet was investigated experimentally. The inlet was of internal compression type with §at walls and rectangular cross section. The experiments were carried out in t

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::92b12584886ad8f3843687f51a9846c3
https://doi.org/10.1051/eucass/201609025

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Two-Dimensional Shock-Wave/Boundary-Layer Interaction in the Presence of Entropy Layer

Autor: Ivan Vladimirovich Egorov, I. V. Struminskaya, A. S. Skuratov, Volf Ya. Borovoy

Publikováno v: AIAA Journal. 51:80-93

Results of experimental and numerical study of gas flow and heat transfer in the region of interference of the impinging oblique shock wave with the near-wall flow on sharp and blunt plates are presented. The study is performed for the freestream Mac

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::c515818e7468285c62cdd4f50bbf06b8
https://doi.org/10.2514/1.j051496

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Two-dimensional interaction between an incident shock and a turbulent boundary layer in the presence of an entropy layer

Autor: A. S. Skuratov, A. Yu. Noev, I. V. Struminskaya, Ivan Vladimirovich Egorov, V. Ya. Borovoi

Publikováno v: Fluid Dynamics. 46:917-934

The results of an experimental and numerical investigation of flow and heat transfer in the region of the interaction between an incident oblique shock and turbulent boundary layers on sharp and blunt plates are presented for the Mach numbers M∞ =

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::7054b0a6e8d54f29440c0960eac94cf8
https://doi.org/10.1134/s0015462811060093

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