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|