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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:	Propellers, Aerial > Evaluation. Airplanes > Turbine-propeller engines.

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Call Number:	NAS 1.26:3047
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Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.26:3047
NAS 1.26:3047	Available Place a Hold