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Fea Modeling from Start to Finish Webinar ºÝºÝߣs

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Aswin John

This webinar covers the geometry import, editing, and idealization of a structural bracket. The bracket then has loads, properties, and boundary conditions defined before meshing. This presentation includes related webinar material. You can view all our webinars at https://structures.aero/webinar/

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5/22/2012 Page 1 Part 1: Preprocessing and Analysis IN THIS WEBINAR: • Geometry import and editing • Meshing and Applying loads • Running a static analysis FEA Modeling from Start to Finish David Cross, Ph.D. Senior Aerospace Stress Engineer Structural Design and Analysis david@structures.aero PRESENTED BY:
5/22/2012 Page 2STRUCTURES.AERO Agenda 1. Analyze support brackets mounted to exterior of a pressure vessel. 2. Begin with a breakout orthogrid panel section and utilize enforced displacements to simulate the internal pressure. 3. Mid-surface the bracket geometry and mesh the bracket mid-surfaces. 4. Model the various connections between the brackets and the orthogrid panel. 5. Define the boundary conditions, enforced displacements, and loads, and use data surface to create load set combinations. 6. Create the linear static analysis set.
5/22/2012 Page 3STRUCTURES.AERO Analyze support brackets mounted to the exterior of a pressure vessel
5/22/2012 Page 4STRUCTURES.AERO Begin with a breakout orthogrid panel section and utilize enforced displacements to simulate the internal pressure View this webinar to learn more about breakout models (submodeling).
5/22/2012 Page 5STRUCTURES.AERO Mid-surface the bracket geometry and mesh To learn more about editing geometry and meshing in Femap, watch the webinar below or read the associated blog post.
5/22/2012 Page 6STRUCTURES.AERO Model the various connections between the brackets and the orthogrid panel On this step we will utilize a custom API. To learn more about API’s, view the introductory webinar or visit the Femap API page on our website.
5/22/2012 Page 7STRUCTURES.AERO Define the boundary conditions, enforced displacements, and loads, and use data surface to create load set combinations. Use data surface to create load set combinations Learn more about load spreading and the data surface editor in the webinar: Load Spreading in Femap
5/22/2012 Page 8STRUCTURES.AERO Create the linear static analysis set This webinar shows the preparation of a model for analysis and conducting a run with the NX Nastran solver.
5/22/2012 Page 9STRUCTURES.AERO Part 2 of the Webinar Series - Postprocessing Tuesday, January 10th, 2PM EST We will cover: • Enveloping results • Post-processing Toolbox • Creating a stress margin plot • Using the Data Table https://structures.aero/fea-modeling-start-finish/
5/22/2012 Page 10STRUCTURES.AERO Structural Design and Analysis (Structures.Aero) Structural Analysis Software from the Engineers Who Use It
5/22/2012 Page 11STRUCTURES.AERO Free tour of Piper Aircraft Femap Symposium Tuesday, January 17th at Piper Aircraft Vero Beach, Florida • VIP Tour of Piper Aircraft • Talk with the Femap Development Team • Presentations on the creation of the Piper M600 More information at https://structures.aero/femap-symposium/
5/22/2012 Page 12STRUCTURES.AERO For questions on the material covered today, please contact David Cross. For questions about pricing, or to see a demo, please contact Marty Sivic. Questions? Marty Sivic Director of Sales msivic@structures.aero 724-382-5290 David Cross, Ph.D. Senior Aerospace Stress Engineer david@structures.aero 703-673-1125

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Fea Modeling from Start to Finish Webinar ºÝºÝߣs

  • 1. 5/22/2012 Page 1 Part 1: Preprocessing and Analysis IN THIS WEBINAR: • Geometry import and editing • Meshing and Applying loads • Running a static analysis FEA Modeling from Start to Finish David Cross, Ph.D. Senior Aerospace Stress Engineer Structural Design and Analysis david@structures.aero PRESENTED BY:
  • 2. 5/22/2012 Page 2STRUCTURES.AERO Agenda 1. Analyze support brackets mounted to exterior of a pressure vessel. 2. Begin with a breakout orthogrid panel section and utilize enforced displacements to simulate the internal pressure. 3. Mid-surface the bracket geometry and mesh the bracket mid-surfaces. 4. Model the various connections between the brackets and the orthogrid panel. 5. Define the boundary conditions, enforced displacements, and loads, and use data surface to create load set combinations. 6. Create the linear static analysis set.
  • 3. 5/22/2012 Page 3STRUCTURES.AERO Analyze support brackets mounted to the exterior of a pressure vessel
  • 4. 5/22/2012 Page 4STRUCTURES.AERO Begin with a breakout orthogrid panel section and utilize enforced displacements to simulate the internal pressure View this webinar to learn more about breakout models (submodeling).
  • 5. 5/22/2012 Page 5STRUCTURES.AERO Mid-surface the bracket geometry and mesh To learn more about editing geometry and meshing in Femap, watch the webinar below or read the associated blog post.
  • 6. 5/22/2012 Page 6STRUCTURES.AERO Model the various connections between the brackets and the orthogrid panel On this step we will utilize a custom API. To learn more about API’s, view the introductory webinar or visit the Femap API page on our website.
  • 7. 5/22/2012 Page 7STRUCTURES.AERO Define the boundary conditions, enforced displacements, and loads, and use data surface to create load set combinations. Use data surface to create load set combinations Learn more about load spreading and the data surface editor in the webinar: Load Spreading in Femap
  • 8. 5/22/2012 Page 8STRUCTURES.AERO Create the linear static analysis set This webinar shows the preparation of a model for analysis and conducting a run with the NX Nastran solver.
  • 9. 5/22/2012 Page 9STRUCTURES.AERO Part 2 of the Webinar Series - Postprocessing Tuesday, January 10th, 2PM EST We will cover: • Enveloping results • Post-processing Toolbox • Creating a stress margin plot • Using the Data Table https://structures.aero/fea-modeling-start-finish/
  • 10. 5/22/2012 Page 10STRUCTURES.AERO Structural Design and Analysis (Structures.Aero) Structural Analysis Software from the Engineers Who Use It
  • 11. 5/22/2012 Page 11STRUCTURES.AERO Free tour of Piper Aircraft Femap Symposium Tuesday, January 17th at Piper Aircraft Vero Beach, Florida • VIP Tour of Piper Aircraft • Talk with the Femap Development Team • Presentations on the creation of the Piper M600 More information at https://structures.aero/femap-symposium/
  • 12. 5/22/2012 Page 12STRUCTURES.AERO For questions on the material covered today, please contact David Cross. For questions about pricing, or to see a demo, please contact Marty Sivic. Questions? Marty Sivic Director of Sales msivic@structures.aero 724-382-5290 David Cross, Ph.D. Senior Aerospace Stress Engineer david@structures.aero 703-673-1125