Cover Image

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.

Saved in:

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.

Description
Summary:	NASA thesaurus headings: Counter rotation - Propeller blades - Vibratory loads - Angular distribution - Fairey aircraft - Propeller slipstreams.
Abstract:	This report presents the results of a propeller vibratory stress survey on the Fairey Gannet aircraft aimed at giving an assessment of the difference in vibratory response between single and counter-rotating propeller operation in angular inflow. The survey showed that counter-rotating operation of the propeller had the effect of increasing the IP response of the rear propeller by approximately 25 percent over comparable single-rotation operation while counter-rotating operation did not significantly influence the IP response of the front propeller.
Item Description:	Distributed to depository libraries in microfiche.
Physical Description:	iii/iv, 73/74 pages : illustrations.
Bibliography:	Includes bibliographical references (page 23/24)
Reproduction Note:	Microfiche.
Funding Information Note:	NASA contract