Formulation and Application of a Stochastic Fatigue Damage Accumulation Model for the Response of Buckled Composite Panels
暂无分享,去创建一个
M. P. Mignolet | M. Mignolet | P. Chen | D. Liu | P. C. Chen | D. D. Liu
[1] Rimas Vaicaitis,et al. Prediction of statistical dynamics of thermally buckled composite panels , 1998 .
[2] J. N. Reddy,et al. A generalization of two-dimensional theories of laminated composite plates† , 1987 .
[3] J. Reddy,et al. Stability and vibration of isotropic, orthotropic and laminated plates according to a higher-order shear deformation theory , 1985 .
[4] C. Ng,et al. Nonlinear and snap-through responses of curved panels to intense acoustic excitation , 1989 .
[5] P. Spanos,et al. Random vibration and statistical linearization , 1990 .
[6] Chuh Mei,et al. Numerical simulation of acoustically induced nonlinear vibrations of a plate with temperature gradient , 1995 .
[7] John Lee,et al. Random Vibration of Thermally Buckled Plates: II Nonzero Temperature Gradient Across the Plate Thickness , 1997 .
[8] R. Vaicaitis,et al. NONLINEAR RESPONSE OF COMPOSITE PANELS TO RANDOM EXCITATION , 1993 .
[9] Jon Lee,et al. Large-Amplitude Plate Vibration in an Elevated Thermal Environment , 1992 .
[10] Paul Malliavin,et al. Stochastic Analysis , 1997, Nature.
[11] Darrell F. Socie,et al. Simple rainflow counting algorithms , 1982 .
[12] Rimas Vaicaitis,et al. Nonlinear Response and Sonic Fatigue of National Aerospace Space Plane Surface Panels , 1994 .