Zobrazeno 1 - 10
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pro vyhledávání: '"N.M. Savin"'
Axial compressor blade cascade design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9ff22c31498dd35aa744c4612f2c7078
Autor:
V.V. Klyuchnikov, Menshikov, Vasiliy, M.E. Olshansky, N.M. Savin, Skob, Yurii, Ugryumov, Mykhaylo
Axial compressor blade design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a5f5bc9d928cab38af75f0bbe141c4a4
Методика пространственного профилирования дозвуковых венцов осевых компрессоров в области сопряжения пера лопаток с торцевой поверхн
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::484e6fb93839da4302c65b03a39bf080
Autor:
V.E. Saren, N.M. Savin
Publikováno v:
UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES ISBN: 1402042671
Results of researches of blade rows unsteady interaction in the three-rows stage of the axial compressor are presented with the purpose of definition the gasdynamical mechanism of clocking effects in system of rows stator-rotor-stator. Experiments we
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ada2e53c49116ca494d7df31cf637a01
https://doi.org/10.1007/1-4020-4605-7_42
https://doi.org/10.1007/1-4020-4605-7_42
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::09f76218034532b396a58f3457bf524e
https://doi.org/10.2514/6.1999-2383
https://doi.org/10.2514/6.1999-2383
Publikováno v:
International Journal of Turbo and Jet Engines. 16
Axial compressors have inherently unsteady flow fields because of relative motion between rotor and stator airfoils. This relative motion leads to viscous and inviscid (potential) interactions between blade rows. As the number of stages increases in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::604bebeaac1442a47ab0d1ca208137a2
https://doi.org/10.1515/tjj.1999.16.3.149
https://doi.org/10.1515/tjj.1999.16.3.149
Publikováno v:
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ddeefaa406a16b959bfa3e9f56ff93e8
https://doi.org/10.2514/6.1998-3413
https://doi.org/10.2514/6.1998-3413
Publikováno v:
International Journal of Turbo and Jet Engines. 15
An experimental and computational research program has been performed to study the effects of stator indexing (clocking) in a high-speed axial compressor stage with an inlet guide vane. The work is directed at determining the basic flow mechanisms ca
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1369f6d828d7e8bc93183a0d7fd6fd96
https://doi.org/10.1515/tjj.1998.15.4.235
https://doi.org/10.1515/tjj.1998.15.4.235
Publikováno v:
Unsteady Aerodynamics and Aeroelasticity of Turbomachines ISBN: 9789401061162
The unsteady flowfield in an axial compressor stage (with an inlet guide vane) has been examined experimentally and computationally. In particular, the effects produced by mutually shifting (clocking) the airfoils in the stationary blade rows has bee
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::72b621faeabd902bf1b08ec6fe2fd90e
https://doi.org/10.1007/978-94-011-5040-8_27
https://doi.org/10.1007/978-94-011-5040-8_27
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