Investigation of a transonic turbine designed for a maximum rotor-blade suction-surface relative Mach number of 1.57
Description: From Summary: "A transonic turbine designed for a maximum blade-surface relative Mach number of 1.57 was investigated experimentally. The performance of the turbine is compared with that of three other transonic turbines that were previously investigated."
Date: October 11, 1954
Creator: Whitney, Warren J.; Wong, Robert Y. & Monroe, Daniel E.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department