Kent Lawrence's ANSYS Tutorial Release 9 PDF

By Kent Lawrence

ISBN-10: 1585032549

ISBN-13: 9781585032549

The 9 classes during this booklet introduce the reader to potent finite aspect challenge fixing through demonstrating using the great ANSYS FEM software program in a chain of step by step tutorials. themes lined contain difficulties concerning trusses, aircraft tension, airplane pressure, axisymmetric and 3-dimensional geometries, beams, plates, conduction and convection warmth move, thermal rigidity, and extra. The tutorials are compatible for both specialist or pupil use. desk of Contents Lesson 1 - Trusses Lesson 2 - aircraft tension, airplane pressure Lesson three - Axisymmetric difficulties Lesson four - three-d difficulties Lesson five - Beams Lesson 6 - Plates Lesson 7 - warmth move, Thermal tension Lesson eight - p-Method Lesson nine - chosen issues

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04S 1. 413 SOI 4 . S3 Figure 2-15 Element SX stresses. The minimum, SMN, and maximum, SMX, stresses as well as the color bar legend give an overall evaluation of the SX stress state. We are interested in the maximum stress at the hole. Use the Zoom to focus on the area with highest stress. Plane Stress / Plane Strain 2-11 Stress variations in the actual isotropic, homogeneous plate should be smooth and continuous across elements. The discontinuities in the SX stress contours above indicate that the number of elements used in this model is too few to accurately calculate the stress values near the hole because of the stress gradients there.

13. Main Menu > Preprocessor > Loads > Define Loads > Apply > Structural > Force/Moment > On Nodes Pick Nodes 1 and 2, Select FY, and Constant value, Enter-300 > OK Figure 1-39 Loads. Let's check the boundary conditions and loads. Use the Utility Menu, top of the screen. 14. Utility Menu > List > Loads > DOF Constraints > On All Nodes Trusses 1-30 Figure 1-40 List constraints. 15. ' - For a visual check: Utility Menu > PlotCtrls turn on Node and Element Numbers (Numbering .. ), and All Applied BCs (Symbols .

The loads, displacement boundary conditions and pressures were applied to the geometry lines. When the solution step was executed, the loads were transferred from the lines to the FEM model nodes. Applying boundary conditions and loads to the geometry facilitates remeshing the problem. The geometry does not change, only the number and location of nodes and elements, and. at solution time, the loads are transferred to the new mesh. Geometry can be created in ANSYS interactively (as was done in the previous tutorial) or it can be created by reading a text file.

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ANSYS Tutorial Release 9 by Kent Lawrence

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