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.
Effect of angular inflow on the vibratory response of a counter-rotating propeller
1985-01-15
Report
No indication
English
Pusher-Propeller Installation Effects in Angular Inflow
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