Aerodynamic design and performance testing of an advanced 30p0s swept, eight bladed propeller at Mach numbers from 0.2 to 0.85
By: D. M. Black, R. W. Menthe, and H. S. Wainauski, United Technologies Corporation ; prepared for Lewis Research Center
Contributors: Menthe, R. W., joint author; Wainauski, H. S., joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; United Technologies Corporation
Series: NASA contractor report ; NASA CR-3047; NASA contractor report -- NASA CR-3047
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 114
Subjects: Propellers, Aerial -- Evaluation; Airplanes -- Turbine-propeller engines
Notes: Contract NAS3-20219

Sept. 1978

Includes bibliographical references