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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.

MARC

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520 3 |a 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. 
520 0 |a NASA thesaurus headings: Counter rotation - Propeller blades - Vibratory loads - Angular distribution - Fairey aircraft - Propeller slipstreams. 
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