Searching Books & More : "United States. National Aeronautics and Space Administration"

Moore, Royce D X
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Performance of a transonic fan stage designed for a low meridional velocity ratio

Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978
Format: Print
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Aerodynamic performance of a 1.35-pressure-ratio axial-flow fan stage

Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978
Format: Print
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Design and overall performance of four highly loaded, high-speed inlet stages for an advanced high-pressure-ratio core compressor

Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978
Format: Print
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Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979
Format: Print
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Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982
Format: Print
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Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979
Format: Print
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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

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980
Format: Print
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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

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982
Format: Print
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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

Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982
Format: Print
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