- Dowell, E.H. and Voss, H.M., Theoretical and experimental panel flutter studies in mach number range 1.0 to 5.0,
AIAA Journal, vol. 3 no. 12
pp. 2292 - 2304 .
(last updated on 2007/04/10)
Paper describes methods and results of coordinated experimental and theoretical investigation of flutter of flat, rectangular, isotropic panels; theoretical calculations are based upon classical, small, deflection-plate theory and three-dimensional, unsteady, aerodynamic theory, as well as simpler theories; effect of dynamics of air in sealed cavity beneath panel is accounted for; experimental program is described, including presentation of pertinent data and comparison with theory.