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Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine

Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine

By Kestutis C. Civinskas

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Publish Date

1984

Publisher

National Aeronautics and Space Administration

Language

eng

Pages

-

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