Theoretical and experimental panel flutter studies in mach number range 1.0 to 5.0

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.

Duke Scholars

Author Earl H. Dowell Thomas Lord Department of Mechanical Engineering and Materia ...