Aerodynamic performance of a 1.20-pressure-ratio fan stage designed for low noise /

by Lewis, G. W. (George W.), 1837-, Moore, Royce D.
Published 1976

Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ̊ /

by Lewis, G. W. (George W.), 1837-, Osborn, Walter Martin, 1918-, Moore, Royce D.
Published 1976

Effect of casing treatment on performance of an inlet stage for a transonic multistage compressor /

by Urasek, Donald C., Lewis, G. W. (George W.), 1837-, Moore, Royce D.
Published 1976

Aerodynamic performance of 0.4066-scale model of JT8D refan stage /

by Moore, Royce D., Kovich, George, Tysl, Edward R.
Published 1976

Design and overall performance of four highly loaded, high-speed inlet stages for an advanced high-pressure-ratio core compressor /

by Reid, Lonnie
Published 1978

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

by Moore, Royce D.
Published 1978

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 /

by Moore, Royce D.
Published 1978

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

by Moore, Royce D.
Published 1979

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 /

by Moore, Royce D.
Published 1982