Nonlinear analysis of aircraft tires via semianalytic finite elements
暂无分享,去创建一个
[1] Ahmed K. Noor,et al. Vibration analysis of laminated anisotropic shells of revolution , 1987 .
[2] Ahmed K. Noor,et al. Analysis of Laminated Anisotropic Shells of Revolution , 1987 .
[3] Bernard Budiansky,et al. Notes on nonlinear shell theory. , 1968 .
[4] Phillip L. Gould,et al. Free Vibration of Shells of Revolution Using FEM , 1974 .
[5] J. L. Sanders,et al. NONLINEAR THEORIES FOR THIN SHELLS , 1963 .
[6] David Bushnell. Analysis of buckling and vibration of ring-stiffened, segmented shells of revolution , 1970 .
[7] H. G. Schaeffer,et al. Nonlinear deflections of asymmetrically loaded shells of revolution. , 1968 .
[8] Joseph Padovan,et al. Complex numerical integration procedure for static loading of anisotropic shells of revolution , 1974 .
[9] G. A. Cohen,et al. FASOR—A second generation shell of revolution code , 1979 .
[10] Ahmed K. Noor,et al. ADVANCES IN CONTACT ALGORITHMS AND THEIR APPLICATION TO TIRES , 1988 .
[11] Ahmed K. Noor,et al. Exploiting symmetries in the modeling and analysis of tires , 1987 .
[12] Ahmed K. Noor,et al. Stress and vibration analyses of anisotropic shells of revolution , 1988 .
[13] Walter Wunderlich,et al. Application of ring elements in the nonlinear analysis of shells of revolution under nonaxisymmetric loading , 1985 .