SOME RECENT CONTRIBUTIONS TO PANEL FLUTTER RESEARCH

5 Donnell, L. EL, "Stability of thin-walled tubes under torsion," NACA Kept. 479, pp. 95-115 (1934). 6 Flugge, W., Stresses in Shells (Springer-Verlag, Berlin, 1962). 7 Green, A. and Zerna, W., Theoretical Elasticity (Oxford University Press, London, 1954). 8 Gerard, G. and Becker, H., "Handbook of structural stability, Part III—Buckling of curved plates and shells," NACA TN 3783 (August 1957). 9 Hess, T. E., "Stability of orthotropic cylindrical shells under combined loading," ARS J. 31, 237-246 (1961). 10 Timoshenko, S. and Gere, J., Theory of Elastic Stability (McGraw-Hill Book Co. Inc., New York, 1961). 11 Love, A. E., A Treatise on the Mathematical Theory of Elasticity (Dover Publications, New York, 1944). 12 March, H. W., Norris, C. B., Smith, C. B., and Kuenzi, E. W., "Buckling of thin-walled plywood cylinders in torsion," Forest Products Lab. Rept. 1529 (June 1945). 13 March, H. W., "Buckling of long, thin plywood cylinders in axial compression," Forest Products Lab. Rept. 1322-A (March 1956). 14 Novozhilov, V. V., The Theory of Thin Shells (P. Noordhoff Ltd., Groningen, The Netherlands, 1959). 15 Von Karman, T. and Tsien, H. S., "The buckling of thin cylindrical shells under axial compression," J. Aeronaut. Sci. 8,303-312(1941). 16 Ho, B. P. C. and Cheng, S., "Some problems in stability of heterogeneous aeolotropic cylindrical shells under combined loading," AIAA J. (to be published).

[1]  Edith F. Farkas,et al.  Flutter of two-bay flat panels of infinite span at supersonic mach numbers , 1965 .

[2]  S. C. Dixon,et al.  Experimental Investigation at Mach Number 3.0 of the Effects of Thermal Stress and Buckling on the Flutter of Four-Bay Aluminum Alloy Panels with Length-Width Ratios of 10 , 1961 .

[3]  Yuan-Cheng Fung,et al.  An introduction to the theory of aeroelasticity , 1955 .

[4]  Robert W. Leonard,et al.  On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders , 1956 .

[5]  John W. Miles,et al.  On the Aerodynamic Instability of Thin Panels , 1956 .

[6]  Eldon E. Kordes,et al.  Flutter research on skin panels , 1960 .

[7]  M. H. Lock,et al.  COMPARATIVE EXPERIMENTAL AND THEORETICAL STUDIES OF THE FLUTTER OF FLAT PANELS IN A LOW SUPERSONIC FLOW , 1961 .

[8]  R. D. Stepanov.  On the Flutter of Cylindrical Shells and Panels Moving in a Flow of Gas , 1958 .

[9]  J. Presnell.  SUPERSONIC PANEL FLUTTER TEST RESULTS FOR FLAT FIBER-GLASS SANDWICH PANELS WITH FOAMED CORES , 1961 .

[10]  M. Holt.  Supersonic Panel Flutter of a Cylindrical Shell of Finite Length , 1961 .

[11]  Eldon E. Kordes,et al.  FLIGHT FLUTTER RESULTS FOR FLAT RECTANGULAR PANELS , 1962 .

[12]  Supersonic flutter of a circular cylindrical shell of finite length in an axisymmetrical mode , 1965 .

[13]  M. J. Lighthill,et al.  Oscillating Airfoils at High Mach Number , 1953 .

[14]  John W. Miles,et al.  Supersonic Flutter of a Cylindrical Shell , 1957 .

[15]  H. Voss,et al.  The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical Shells , 1961 .

[16]  Holt Ashley,et al.  Piston Theory-A New Aerodynamic Tool for the Aeroelastician , 1956 .

[17]  Y. C. Fung,et al.  On the Vibration of Thin Cylindrical Shells Under Internal Pressure , 1957 .

[18]  H. J. Cunningham,et al.  Experimental and theoretical studies of panel flutter at Mach numbers 1.2 to 3.0 , 1955 .

[19]  Maurice A. Sylvester,et al.  Some Experimental Studies of Panel Flutter at Mach Number 1.3 , 1957 .

[20]  John W. Miles,et al.  ON PANEL FLUTTER IN THE PRESENCE OF A BOUNDARY LAYER , 1959 .

[21]  J. Miles.  The Aerodynamic Forces on an Oscillating Flap at Supersonic Speeds , 1947 .

[22]  James Doyle McClure,et al.  On perturbed boundary layer flows , 1962 .