Advanced turboprop wing installation effects measured by unsteady blade pressure and noise [microform] / 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.

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Bibliographic Details
Main Author:	Heidelberg, Laurence J.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Woodward, Richard P.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], [1987]
Series:	NASA technical memorandum ; 100200.
Subjects:	Airplanes > Wings. Compressor blades. Engine noise. Installing. Pressure distribution. Propellers. Turboprop engines. Unsteady flow. Wings.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:100200
NAS 1.15:100200	Restricted Place a Hold