Aerodynamic design and performance testing of an advanced [30 degree] swept, eight bladed propeller at Mach numbers from 0.2 to 0.85 / D. M. Black, R. W. Menthe, and H. S. Wainauski, United Technologies Corporation ; prepared for Lewis Research Center.

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Bibliographic Details
Online Access: Search for the full-text version of this title in HathiTrust
Main Author: Black, D. M.
Corporate Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, United Technologies Corporation
Other Authors: Wainauski, H. S., Menthe, R. W.
Format: Government Document Book
Language:English
Published: [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978.
Series:NASA contractor report ; NASA CR-3047.
Subjects:

MARC

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245 1 0 |a Aerodynamic design and performance testing of an advanced [30 degree] swept, eight bladed propeller at Mach numbers from 0.2 to 0.85 /  |c D. M. Black, R. W. Menthe, and H. S. Wainauski, United Technologies Corporation ; prepared for Lewis Research Center. 
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500 |a Sept. 1978. 
504 |a Includes bibliographical references. 
650 0 |a Propellers, Aerial  |x Evaluation. 
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