Analysis of high Reynolds number inviscid/viscid interactions in cascades | Zendy

Mark A. Barnett | Zendy; Joseph M. Verdon | Zendy; Timothy C. Ayer | Zendy

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Analysis of high Reynolds number inviscid/viscid interactions in cascades

Author(s) -

Mark A. Barnett,

Joseph M. Verdon,

Timothy C. Ayer

Publication year - 1993

Publication title -

aiaa journal

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.828

H-Index - 158

eISSN - 1081-0102

pISSN - 0001-1452

DOI - 10.2514/3.11879

Subject(s) - inviscid flow , mechanics , turbomachinery , reynolds number , wake , shock (circulatory) , prandtl number , flow (mathematics) , turbulent prandtl number , boundary layer , physics , trailing edge , turbulence , heat transfer , nusselt number , medicine

An efficient analysis for predicting steady, strong, inviscid/viscid interaction phenomena, such as viscous-layer separation, shock/bonndary-layer interaction, and trailing-edge/near-wake interaction, in turbomachinery blade passages is needed as part of a comprehensive analytical blade design prediction system. Such an analysis is described in the present paper. It uses an invicid/viscid interaction approach, in which the flow in the outer inviscid region is assumed to be potential and the flow in the inner or viscons-layer region is governed by Prandtl's equations

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