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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

Published Year

• 1950-1959 (4) *

Subject

• Axial flow compressors--Blades (4) *
• Cascades (Fluid dynamics) (3)
• Aerofoils (1)
• Axial flow compressors--Aerodynamics (1)
• Compressors--Blades (1)
• Compressors--Performance (1)
• Gas-turbines--Blades (1)
• Reynolds number (1)

Author

• Emery, James C. (2)
• Erwin, John R. (2)
• Savage, Melvyn. (2)
• Ashby, George C. (1)
• Felix, A. Richard. (1)
• Schulze, Wallace M. (1)

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