Papers Published

  1. Dowell, E.H., Nonlinear oscillations of fluttering plate -- 2, AIAA Journal, vol. 5 no. 10 (1967), pp. 1856 - 1862 .
    (last updated on 2007/04/10)

    Abstract:
    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.

    Keywords:
    Flutter;