Investigation of a high-performance axial-flow compressor transonic inlet rotor designed for 37.5 pounds per second per square foot of frontal area 1: aerodynamic design and overall performance
Description: Report presenting an investigation of the design and tests of a transonic inlet rotor with emphasis placed on increasing the design specific weight flow while maintaining reasonably high pressure ratio and efficiency. Information regarding peak efficiency and how to best achieve it through design is provided.
Date: March 24, 1955
Creator: Savage, Melvyn & Felix, A. Richard
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department