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Royce D Moore

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TurbomachinesPerformance 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 2.05Royce D Moore

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

Royce D Moore · National Aeronautics and Space Administration, Scientific and Technical Information Branch

113 sayfa · 1982

Aerodynamics / Compressors / Turbomachines

TurbomachinesPerformance 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 1.82Royce D Moore

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

Royce D Moore · National Aeronautics and Space Administration, Scientific and Technical Information Branch

111 sayfa · 1982

Aerodynamics / Compressors / Turbomachines

TurbomachinesPerformance 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 2.05Royce D Moore

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

Royce D Moore · National Aeronautics and Space Administration, Scientific and Technical Information Office

101 sayfa · 1978

Aerodynamics / Compressors / Turbomachines

TurbomachinesAerodynamic performance of axial-flow fan stage operated at nine inlet guide vane anglesRoyce D Moore

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles

Royce D Moore · For sale by the National Technical Information Service]

40 sayfa · 1979

Performance / Aerodynamics / Fans (Machinery) / Turbomachines

TurbomachinesPerformance of a transonic fan stage designed for a low meridional velocity ratioRoyce D Moore

Performance of a transonic fan stage designed for a low meridional velocity ratio

Royce D Moore · for sale by the National Technical Information Service

80 sayfa · 1978

Compressors / Turbomachines

VanesDetailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnelRoyce D. Moore

Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

Royce D. Moore · Lewis Research Center

148 sayfa · 1987

Cascades / Corner flow / Wind tunnels / Vanes

Wind tunnel modelsExperimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnelRoyce D. Moore

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

Royce D. Moore · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1986

Wind tunnel models

Rotors (Helicopters)Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stageRoyce D Moore

Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage

Royce D Moore · National Aeronautics and Space Administration, Scientific and Technical Information Branch

85 sayfa · 1982

Impellers / Dynamics / Rotors (Helicopters)

TurbomachinesAerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stageRoyce D Moore

Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage

Royce D Moore · For sale by the National Technical Information Service]

68 sayfa · 1979

Performance / Aerodynamics / Fans (Machinery) / Turbomachines

Supersonic transport planesNASA Lewis supersonic throughflow fan programRoyce D. Moore

NASA Lewis supersonic throughflow fan program

Royce D. Moore · National Aeronautics and Space Administration

Sayfa sayısı yok · 1990

Supersonic transport planes