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Effect of angular inflow on the vibratory response of a counter-rotating propeller [microform] : by J.E. Turnberg, P.C. Brown.

NASA thesaurus headings: Counter rotation - Propeller blades - Vibratory loads - Angular distribution - Fairey aircraft - Propeller slipstreams.

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Bibliographic Details
Main Author:	Turnberg, J. E.
Corporate Authors:	United States. National Aeronautics and Space Administration, United Technologies Corporation. Hamilton Standard Division
Other Authors:	Brown, P. C.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Windsor Locks, CT] : [Springfield, Va.] : [Hamilton Standard Div., United Technologies Corp. ; [Washington, DC] : NASA ; [For sale by the National Technical Information Service], [1985]
Series:	NASA contractor report ; NASA CR-174819.
Subjects:	Fairey aircraft. Counter rotation. Propeller blades. Vibratory loads.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:174819
NAS 1.26:174819	Restricted Place a Hold