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- Performance of compressor blade cascades at high Mach numbers
- 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
- Analysis of aerodynamic blade-loading-limit parameters for NACA 65-(C[sub zeta]₀A₁₀) 10 compressor-blade sections at low speeds