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Low-speed cascade tests of two 45 degree swept compressor blades with constant spanwise loading

Description: Report discussing an investigation of two 45 degree swept blades in low-speed cascade tunnels at a range of angles of attack and various combinations of inlet-air angle and solidity. The isolated wing method used to design the blade predicted the twist distribution and camber shape necessary to obtain an almost uniform spanwise loading.
Date: March 15, 1954
Creator: Beatty, Loren A.; Savage, Melvyn & Emery, James C.
Partner: UNT Libraries Government Documents Department