R. D. Moore

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

L. Reid, R. D. Moore · NASA Technical Reports Server (NASA) · 1978 · 323 citations

Engineering, Aerospace Engineering, Design Optimization +14

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

R. D. Moore, L. Reid · NASA STI Repository (National Aeronautics and Space Administration) · 1980 · 142 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +13

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 1.82

L. Reid, R. D. Moore · NASA Technical Reports Server (NASA) · 1978 · 82 citations

Engineering, Aerospace Engineering, Mechanical Engineering +13

Method for prediction of pump cavitation performance for various liquids, liquid temperatures, and rotative speeds

R. D. Moore, Robert S. Ruggeri · NASA Technical Reports Server (NASA) · 1969 · 70 citations

Engineering, Mechanical Engineering, Physics +16

Effect of casing treatment on overall and blade element performance of a compressor rotor

R. D. Moore, G. Kovich, Robert J. Blade · NASA Technical Reports Server (NASA) · 1971 · 60 citations

Engineering, Mechanical Engineering, Experimental Performance +12