Description: Report presenting a new blade series designed to operate at near choking inlet Mach numbers and to have near maximum critical Mach numbers by employing high aerodynamic loading of the profiles in the leading-edge region and relatively straight trailing edges. Results regarding the aerodynamic characteristics and prediction of high-speed performance are provided.
Date: November 26, 1954
Creator: Dunavant, James C.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department