- Dowell, E.H., Nonlinear oscillations of fluttering plate -- 2,
AIAA Journal, vol. 5 no. 10
pp. 1856 - 1862 .
(last updated on 2007/04/10)
Quasi-steady aerodynamic theory; Galerkin's method is used to reduce mathematical problem to system of nonlinear, ordinary, integral-differential equations in time, which are solved by numerical integrations; results are presented for limit cycle deflection and frequency as functions of dynamic pressure; air/panel mass ratio; length-to-width ratio a/b; and Mach number.