NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results

George C. Ashby, Jr, John R. Erwin, Wallace M. Schulze
naca-tn-4130
Oct 1057


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 with the annulus area varied were corrected to the two-dimensional-flow condition by two methods.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-tn-4130.pdf