Investigation formulates flutter problem of wing aileron tab combination with aerodynamic overhang in terms of system of six linear ordinary differential equations of motion with constant coefficients.
Two-dimensional transient motion and flutter of wing having four degrees of freedom
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 8
1952
3 pages
Article (Journal)
English
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Engineering Index Backfile | 1954
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