A brief description is given of one approach taken by a manufacturer of light business and personal aircraft to the flutter analysis of propeller whirl flutter, twin-boom aircraft, T-tail configuration, servo tabs, and all-moving tail. Effects of structural variations that may occur in the service life of an aircraft are presented, and the effect of ice formation on control surfaces is discussed.
Some Special Investigation Areas in Light Aircraft Flutter
Sae Technical Papers
National Business Aircraft Meeting and Engineering Display ; 1972
1972-02-01
Aufsatz (Konferenz)
Englisch
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