Download ANSYS Tutorial Release 9 by Kent Lawrence PDF

By Kent Lawrence

ISBN-10: 1585032549

ISBN-13: 9781585032549

The 9 classes during this booklet introduce the reader to powerful finite aspect challenge fixing via demonstrating using the excellent ANSYS FEM software program in a sequence of step by step tutorials. themes coated comprise difficulties regarding trusses, airplane rigidity, airplane pressure, axisymmetric and third-dimensional geometries, beams, plates, conduction and convection warmth move, thermal pressure, and extra. The tutorials are appropriate for both expert or scholar use. desk of Contents Lesson 1 - Trusses Lesson 2 - aircraft pressure, airplane pressure Lesson three - Axisymmetric difficulties Lesson four - 3-dimensional difficulties Lesson five - Beams Lesson 6 - Plates Lesson 7 - warmth move, Thermal tension Lesson eight - p-Method Lesson nine - chosen themes

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Extra resources for ANSYS Tutorial Release 9

Sample text

375 inch from the right edge. If you are not using an IGES file to define the geometry for this exercise, you can create the geometry directly in ANSYS with key points, lines, arcs by selecting File > Read Input from to read in the text file given below and skipping the IGES import steps 2, 3, 4, and 10 below. /FILNAM,Seatbelt /title, Seatbelt Geometry ! 0, 0 0 !

However, the horizontal link could also buckle in the X-Z plane, that is, in a direction normal to the plane of analysis. The end conditions are not pinned for this mode of deformation but probably not quite completely fixed either, so this would require further investigation on the part of the stress analyst. To obtain the support reactions 13. Main Menu > General Postproc > List Results > Reaction Solution > All items > OK At any point you can save your work using the ANSYS binary file format.

Finally, in doing this computation we will include the Solution and Postprocessing instruction in the text file and not perform those steps interactively as we did in the previous tutorial. 1. Prepare Input File /FILNAM,T1B /title, Simple Truss w Composite Tube /prep7 et, 1, linkl ! 1 is linkl ! 27 ! Material Properties: E for material no. 1 ! l ! 3 ! Material Properties: E for material no. 2 ! 2 Trusses 1-19 f, 1, fy, -300. Force at node 1 in y-dlrection is -300. f, 2, fy, -300. Force at node 2 in y-direction is -300.

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ANSYS Tutorial Release 9 by Kent Lawrence


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