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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 pressu - Royce D Moore
Performance of a low-pressure fan stage with reverse flow (NASA technical memorandum) - Royce D Moore
Aerodynamic performance of 0.4066-scale model of JT8D refan stage (NASA technical memorandum ; NASA TM X-3356) - Royce D Moore
Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet (NASA technical memorandum ; NASA TN D-8458) - Royce D Moore
Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment (NASA technical memorandum ; NASA TM X-3479) - Royce D Moore
Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles (NASA technical paper) - Royce 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 pressu - Royce D Moore
Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage (NASA technical paper) - Royce D Moore
Aerodynamic performance of a 1.25-pressure-ratio axial-flow fan stage (NASA technical memorandum) - Royce D Moore