Analyzing thick and thin domains is quick and easy with StressCheck’s Modal & Buckling Solver module. In most cases only one element is needed through a part’s thickness for a reliable solution. The computed natural frequencies and buckling load factors exhibit superconvergence. Pre-stress conditions can be easily handled.
Modal & Buckling Solver
The Modal & Buckling Solver provides a solver and post-processing functionalities for modal analysis and bifurcation (eigenvalue) buckling. Modal and buckling analyses can be performed for both 2D planar problems (plates and beam elements) and 3D problems (shell, extrude and solid elements).
Key Features and Advantages
Modal analysis supports computation of natural frequencies and their associated mode shapes.
- Mass density may be defined as a constant or as a formula
- Mode shapes can be constrained or unconstrained, in which the first six shapes are rigid body modes
- Can specify a pre-stress for 3D problems to account for initial stress conditions
Buckling analysis supports computation of buckling load factors and their associated buckling mode shapes. Both standard and pre-load buckling options are incorporated. To perform a buckling analysis, StressCheck first solves the linear problem corresponding to the specified loads and constraints. Using the stress field computed from the linear solution, a geometric stiffness matrix is generated and used for eigenvalue computation.
- Standard buckling provides a buckling load factor for a given loading condition
- Pre-load buckling takes into account an additional fixed set of loads (for example, residual stresses) when reporting the buckling factor for applied loads
- StressCheck’s high-order elements minimize detrimental locking effects on the eigenvalue solution and promote proper simulation of mode shapes
- The element formulation permits rapid transitions from thin to thick domains
- In many cases only one element is needed through a part thickness
- Convergence information for natural frequencies and buckling load factors is reported
- No limit on number of eigenvalues to be computed
- StressCheck Handbook simplifies boundary condition influence on buckling load factor and mode shapes by allowing users to switch between support types
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“The addition of incremental theory of plasticity in StressCheck has greatly improved our ability to accurately predict the fatigue life of joints with interference fit fasteners and cold worked holes. This ability is especially important, not only in support of maintaining aging aircraft but also in analyzing some of the new cold working techniques that have been introduced in recent years.
Prior to this implementation, analysts often relied on closed-form approximations or simple factors that were often overly conservative and sometimes even unconservative when used in life prediction. Now, not only can we more accurately predict residual stresses in these complex structural joints, but we can also do so in a timely manner given the modeling and analysis efficiency that exists with a p-version FEA code such as StressCheck.”F-15 Structures Manager
The Boeing Company