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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.
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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)
