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EFFECTS OF STATOR CLOCKINGINSYSTEMOF ROWS STATOR-ROTOR-STATOROF THE SUBSONICAXIAL COMPRESSOR

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

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Full-annulus simulations of airfoil clocking in a compressor at off-design operating conditions

Autor: Douglas L. Sondak, V.E. Saren, Paul G. A. Cizmas, Daniel J. Dorney, N.M. Savin

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

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Full-Annulus Simulations of Airfoil Clocking in a 1-1/2 Stage Axial Compressor

Autor: Daniel J. Dorney, V.E. Saren, Paul G. A. Cizmas, Douglas L. Sondak, N.M. Savin

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

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Experimental and numerical investigation of airfoil clocking and inter-blade-row gap effects on axial compressor performance

Autor: Douglas L. Sondak, N.M. Savin, V.E. Saren, Daniel J. Dorney

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

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Experimental and Numerical Investigation of Airfoil Clocking and Inner-Blade-Row Gap Effects on Axial Compressor Performance

Autor: N.M. Savin, D.L. Son, Daniel J. Dorney, V.E. Saren

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

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Experimental and Numerical Investigation of Unsteady Rotor-Stator Interaction on Axial Compressor Stage (with IGV) Performance

Autor: V.E. Saren, Daniel J. Dorney, N.M. Savin, R. M. Zacharias

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

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