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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 typical axial-flow compressor rotor using NACA 65-series compressor blades was tested at low speeds and its performance was measured over a range of quantity flow rates at several values of annulus-area ratio, blade-setting angle, solidity, and Reynolds number to compare with porouswall cascade results. The data obtained using varying annulus area were corrected to the two-dimensional-flow condition by two methods.
Annual Report of the National Advisory Committee for Aeronautics
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
