
doi: 10.2514/3.60488
For k= 1, i.e., for the case of isotropic core, the critical loads TV* and N*L, given by Eqs. (16) and (17) reduce to those obtained by Fulton. In ord"er to show the effect of orthotropic core upon the critical loads, the following numerical values for shell property and dimensions are used: El =E2 =E, tj = t2 = t=0.05 in., ju = 0.3, E/Gxz = 2xW, 0 = 100 in., # = 200 in., C = 0.5 in. The critical loads are expressed in the following form as
Numerical solution of boundary value problems involving ordinary differential equations, Transonic flows, Finite element, Rayleigh-Ritz and Galerkin methods for boundary value problems involving PDEs, Stability and convergence of numerical methods for boundary value problems involving PDEs, General aerodynamics and subsonic flows
Numerical solution of boundary value problems involving ordinary differential equations, Transonic flows, Finite element, Rayleigh-Ritz and Galerkin methods for boundary value problems involving PDEs, Stability and convergence of numerical methods for boundary value problems involving PDEs, General aerodynamics and subsonic flows
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