Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade
Description:
An investigation has been conducted to compare the performance of NACA 65-series compressor blades in two-dimensional cascade with that in an axial flow compressor. Blade pressure distributions were obtained by the use of a mercury-seal pressure-transfer device. The comparison indicated that cascade data accurately predicted the turning angle and blade pressure distribution obtained in the compressor at design conditions.
Date:
March 1957
Creator:
Westphal, Willard R. & Godwin, William R.
Partner:
UNT Libraries Government Documents Department