Stability equation for structure acted upon by air forces is set up in form convenient for flutter analysis; unrestricted generalized coordinates in complex form are used; expressions given for aerodynamical coefficients of airfoil in terms of theoretical two-dimensional coefficients; mechanical coefficients for airfoils expressed in terms of quantities generally known or easily calculable; value of empirical data from resonance and static deflection tests emphasized.
Three-dimensional flutter analysis
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 9 , n 2
1941
8 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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