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- Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade
- NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results
- A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed
- Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading
- A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05