Advanced turboprop wing installation effects measured by unsteady blade pressure and noise
By: Laurence J. Heidelberg and Richard P. Woodward ; prepared for the 11th Aeroacoustics Conference sponsored by the American Institute of Aeronautics and Astronautics, Sunnyvale, California, October 19-21, 1987.
Contributors: Woodward, Richard P.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 100200.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1987
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 21
Subjects: Airplanes -- Wings.; Compressor blades.; Engine noise.; Installing.; Pressure distribution.; Propellers.; Turboprop engines.; Unsteady flow.; Wings.
Notes: Cover title.

Distributed to depository libraries in microfiche.

"AIAA-87-2719."

Includes bibliographical references (p. 9).

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1987] 1 microfiche : negative.