Advanced turboprop wing installation effects measured by unsteady blade pressure and noise.

Advanced turboprop wing installation effects measured by unsteady blade pressure and noise.

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

Evans: US Documents Microfiche (3rd floor)

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Call Number: NAS 1.15:100200
 
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NAS 1.15:100200 Available