论文信息 - Effects of differential pressure, thermal stress, and buckling on flutter of flat panels with length-width ratio of 2

Effects of differential pressure, thermal stress, and buckling on flutter of flat panels with length-width ratio of 2

distinct flutter boundaries were obtained, one associated with standing- wave flutter and the other with traveling-wave flutter. Standing-wave flutter usually occurred when the differential pressure Ap was less than 0.10 psi; traveling-wave flutter usually occurred when Ap was greater than

S. C. Dixon | C. Shore

[1] S. C. Dixon. APPLICATION OF TRANSTABILITY CONCEPT TO FLUTTER OF FINITE PANELS AND EXPERIMENTAL RESULTS , 1963 .

[2] S. Kobayashi. Flutter of simply supported rectangular panels in a supersonic flow. , 1962 .

[3] 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 .

[4] 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 .

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