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

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Published Year

• 1950-1959 (2)

Subject

• Axial flow compressors--Design and construction (2) *
• Axial flow compressors--Blades--Testing (1)
• Jet engines--Air intakes--Design and construction (1)

Author

• Beatty, Loren A. (1)
• Emery, James C. (1)
• Lewis, George W., (1)
• Savage, Melvyn. (1)
• Schwenk, Francis C. (1)
• Serovy, G. K. (1)

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