Design and Optimization of Tandem Arranged Cascade in a Transonic Compressor

High-Lift Aerodynamics

A. M. O. Smith · Journal of Aircraft · 1975 · 548 citations

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

Effects of Vortex Generator Application on the Performance of a Compressor Cascade

Alexander Hergt, Robert K. Meyer, Karl Engel · Journal of Turbomachinery · 2012 · 119 citations

Engineering, Aerospace Engineering, Mechanical Engineering +15

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