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Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients

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 (3) *

Subject

• Axial flow compressors--Blades (2)
• Aerofoils (1)
• Axial flow compressors--Aerodynamics (1)
• Axial flow compressors--Design and construction (1)
• Cascades (Fluid dynamics) (1)
• Compressors--Blades (1)
• Jet engines--Air intakes--Design and construction (1)

Author

• Savage, Melvyn. (3) *
• Emery, James C. (2)
• Beatty, Loren A. (1)
• Erwin, John R. (1)

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