Automated nose fairing design - Honeycomb sandwich construction

Computer program for near optimum structural designs of ring stiffened honeycomb sandwich nose fairing

Computer program analyzes Buckling Of Shells Of Revolution with various wall construction, BOSOR

Computer program performs stability analyses for a wide class of shells without unduly restrictive approximations. The program uses numerical integration, finite difference of finite element techniques to solve with reasonable accuracy almost any buckling problem for shells exhibiting orthotropic behavior

Influence of imperfections and edge restraint on the buckling of axially compressed cylinders

Edge restraint and imperfection influence on buckling of axially compressed cylinder

Global function approach in structural analysis: Basic approach, numerical results

The structural response to a given environment is described by the differential equations of motion of deformable bodies. Analytic solutions of such problems for a reasonably large class of structural configurations are not within the realm of the possible. Consequently, the mathematical problem is recast into a numerical problem for solution on the computer. New technology in the space and energy fields led to a growing demand for accurate analysis which at times cannot be met due to the limits set by available budgets for computer time. In response to this need for more efficient numerical analysis, the possibilities of reducing the number of freedoms in the system through a revival of the global function approach were explored

Buckling of shells of revolution with various wall constructions. Volume 3 - User's manual for BOSOR

Computer program for analysis of shells of revolution with axisymmetric loadin

Buckling of shells of revolution with various wall constructions. Volume 2 - Basic equations and method of solution

Basic equations and method of solution for computerized analysis of shells of revolution with axisymmetric collapse and nonsymmetric bifurcation buckling behavio

Buckling of shells of revolution with various wall constructions. Volume 1 - Numerical results

Numerical results of buckling of shells of revolution for computer progra