NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results /
Wallace M. Schultze, John R. Erwin, and George C. Ashby, Jr.

APA Citation

Schulze, W. M., Ashby, G. C., Erwin, J. R., Langley Aeronautical Laboratory., United States. National Adviosry Committee for Aeronautics. (1953). NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results. Washington, D.C.: National Advisory Committee for Aeronautics.

MLA Citation

United States. National Adviosry Committee for Aeronautics, et al.. NACA 65-series Compressor Rotor Performance With Varying Annulus-area Ratio, Solidity, Blade Angle, And Reynolds Number And Comparison With Cascade Results. Washington, D.C.: National Advisory Committee for Aeronautics, 1953.