Evaluation of wind tunnel performance testings of an advanced 45⁰ swept eight-bladed propeller at Mach numbers from 0.45 to 0.85
By: C. Rohrbach ... [et al.] ; prepared for Lewis Research Center under contract NAS3-20769
Contributors: Rohrbach, C; Lewis Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; United Technologies Corporation. Hamilton Standard Division
Series: NASA contractor report -- 3505
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 124
Subjects: Transportation -- Energy conservation; Propellers, Aerial -- Testing; Airplanes -- Turbine-propeller engines -- Testing; Mechanical efficiency
Notes: "Hamilton Standard."

STAR category 02

"March 1982"--Cover

Includes bibliographical references