Effects of reset stators and a rotating, grooved stator hub on performance of a 1.92-pressure-ratio compressor stage /

by Lewis, G. W. (George W.), 1837-
Published 1977

Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊ /

by Lewis, G. W. (George W.), 1837-, Kovich, George
Published 1976

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

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

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

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

by Moore, Royce D.
Published 1978