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Last edited by ImportBot
September 19, 2008 | History
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Royce D. Moore

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7 works Add another?

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  • Cover of: Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 2.05

    First published in 1978 3 editions in 1 language
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  • Cover of: Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05

    First published in 1982 3 editions in 1 language
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  • Cover of: Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82

    First published in 1982 3 editions in 1 language
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  • Cover of: Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles

    First published in 1979 1 edition in 1 language — 1 previewable
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  • Cover of: Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

    First published in 1987 1 edition
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  • Cover of: Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

    First published in 1986 1 edition in 1 language
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  • Cover of: NASA Lewis supersonic throughflow fan program

    First published in 1990 1 edition in 1 language
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We need a photo of Royce D. Moore

Subjects
Aerodynamics, Turbomachines, Compressors, Cascades, Corner flow, Fans (Machinery), Performance, Supersonic transport planes, Vanes, Wind tunnel models, Wind tunnels

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ID Numbers

  • OLID: OL4829703A

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History

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September 19, 2008 Created by ImportBot Imported from Oregon Libraries MARC record