Comparison of theory and experiment for nonlinear flutter of loaded plates

Flutter analysis of plates with inplane boundary support flexibility exposed to transverse pressure loading or buckled by uniform thermal expansion

[1]  S. Durvasula,et al.  Flutter of simply supported, parallelogrammic, flat panels in supersonic flow. , 1966 .

[2]  J. H. Argyris,et al.  Matrix displacement analysis of plates and shells , 1966 .

[3]  Kariappa,et al.  Application of matrix displacement methods in the study of panel flutter. , 1969 .

[4]  C. S. Ventres,et al.  Nonlinear flutter of loaded plates. , 1968 .

[5]  S. C. Dixon,et al.  Effects of differential pressure, thermal stress, and buckling on flutter of flat panels with length-width ratio of 2 , 1963 .

[6]  Y. C. Fung,et al.  On Two-Dimensional Panel Flutter , 1958 .

[7]  J. Hedgepeth,et al.  Flutter of Rectangular Simply Supported Panels at High Supersonic Speeds , 1957 .

[8]  Earl H. Dowell,et al.  Modal equations for the nonlinear flexural vibrations of a cylindrical shell , 1968 .

[9]  Earl H. Dowell,et al.  Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0. , 1965 .

[10]  J. G. Eisley,et al.  Flutter of Thin Plates under Combined Shear and Normal Edge Forces , 1963 .

[11]  F. B. Hildebrand,et al.  Methods of Applied Mathematics , 1966 .

[12]  E. Dowell.  Nonlinear oscillations of a fluttering plate. II. , 1966 .

[13]  E. Dowell,et al.  THE EFFECT OF A CAVITY ON PANEL VIBRATION , 1963 .

[14]  C. P. Shore,et al.  Flutter at Mach 3 of thermally stressed panels and comparison with theory for panels with edge rotational restraint , 1966 .

[15]  R. W. Fralich,et al.  Flutter of buckled, simply supported, rectangular panels at supersonic speeds , 1968 .

[16]  S. C. Dixon.  EXPERIMENTAL INVESTIGATION AT MACH NUMBER 3.0 OF EFFECTS OF THERMAL STRESS AND BUCKLING ON FLUTTER CHARACTERISTICS OF FLAT SINGLE-BAY PANELS OF LENGTH-WIDTH RATIO 0.96 , 1962 .