The buckling stress for this case is obtained from the formula. ox = ksE(ts/b)2 (63) The analytical solution plotted in Fig. ... These instability modes and the corresponding mode deflections and rotations used in the analysis are shown in Fig. 7.

Title | : | A collection of technical papers on structural dynamics as related to advanced transportation systems |

Author | : | American Institute of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers |

Publisher | : | - 1972 |

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