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Effect Of Angular Inflow On The Vibratory Response Of A Counter Rotating Propeller by Jay E. Turnberg
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1NASA Technical Reports Server (NTRS) 19870001407: Effect Of Angular Inflow On The Vibratory Response Of A Counter-rotating Propeller
By NASA Technical Reports Server (NTRS)
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.
“NASA Technical Reports Server (NTRS) 19870001407: Effect Of Angular Inflow On The Vibratory Response Of A Counter-rotating Propeller” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19870001407: Effect Of Angular Inflow On The Vibratory Response Of A Counter-rotating Propeller
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19870001407: Effect Of Angular Inflow On The Vibratory Response Of A Counter-rotating Propeller” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - COUNTER ROTATION - PROPELLER BLADES - VIBRATORY LOADS - ANGULAR DISTRIBUTION - FAIREY AIRCRAFT - PROPELLER SLIPSTREAMS - Turnberg, J. E. - Brown, P. C.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19870001407
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 58.25 Mbs, the file-s for this book were downloaded 71 times, the file-s went public at Wed Sep 14 2016.
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