A Criterion for the Prevention of Spring-Tab Flutter
نویسندگان
چکیده
منابع مشابه
Ministry of Supply
This paper gives the results of an investigation into the effects of wing torsion in a ternary-type spring-tab flutter. The results presented are for a series of calculations on an idealised system having degrees of freedom in wing pitch, rotation of the control surface and rotation of the tab; the pitching degree of freedom is spring restrained and is intended to represent wing torsion. The ta...
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تاریخ انتشار 2002