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mdnastran_r3_training_120_notes.pdf

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Part Number: MDNA*R3*Z*Z*Z*SM-NAS120-WBK Copyright 2008 MSC.Software Corporation August 2008 Linear Static, Normal Modes, and Buckling Analysis Using MD Nastran R3 and Patran 2008r1 NAS120 Course Notes MSC.Software Corporation Europe MSC.Software GmbH Am Moosfeld 13 81829 Munich, Germany Telephone: (49) (89) 43 19 87 0 Fax: (49) (89) 43 61 71 6 Corporate MSC.Software Corporation 2 MacArthur Place Santa Ana, CA 92707 USA Telephone: (800) 345-2078 Fax: (714) 784-4056 Asia Pacific MSC.Softwar
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  Part Number: MDNA*R3*Z*Z*Z*SM-NAS120-WBKCopyright  2008 MSC.Software CorporationAugust 2008 Linear Static, Normal Modes, and BucklingAnalysis Using MD Nastran R3 and Patran2008r1 NAS120 Course Notes MSC.Software Corporation Europe MSC.Software GmbHAm Moosfeld 1381829 Munich, GermanyTelephone: (49) (89) 43 19 87 0Fax: (49) (89) 43 61 71 6 Corporate MSC.Software Corporation2 MacArthur PlaceSanta Ana, CA 92707 USATelephone: (800) 345-2078Fax: (714) 784-4056 Asia Pacific MSC.Software Japan Ltd.Shinjuku First West 8F23-7 Nishi Shinjuku1-Chome, Shinjuku-KuTokyo 160-0023, JAPANTelephone: (81) (3)-6911-1200Fax: (81) (3)-6911-1201  2Copyright  2008 MSC.Software Corporation Legal Information MSC.Software Corporation reserves the right to make changes in specifications and other information contained in thisdocument without prior notice. The concepts, methods, and examples presented in this text are for illustrative andeducational purposes only, and are not intended to be exhaustive or to apply to any particular engineering problem ordesign. MSC.Software Corporation assumes no liability or responsibility to any person or company for direct or indirectdamages resulting from the use of any information contained herein.Copyright © 2008 MSC.Software Corporation. All Rights Reserved. This notice shall be marked on any reproduction ofthis documentation, in whole or in part. Any reproduction or distribution of this document, in whole or in part, without theprior written consent of MSC.Software Corporation is prohibited.The MSC.Software corporate logo, Adams, Dytran, Easy5, Fatigue, Laminate Modeler, Marc, Mentat, MD Nastran, Patran,MSC, MSC Nastran, Mvision, Patran, SimDesigner, SimEnterprise, SimManager, SimXpert and Sofy are trademarks orregistered trademarks of the MSC.Software Corporation in the United States and/or other countries. NASTRAN is aregistered trademark of NASA. All other trademarks belong to their respective owners.  3Copyright  2008 MSC.Software Corporation CONTENTS 4-57Workshop 4 “Stadium Truss”3-40Workshop 3 “Editing a Nastran Input File”2-50Workshop 2 “Simply Supported Beam”1-37Workshop 1 “Landing Gear Strut Analysis”4-48Post Processing CROD Results4-19The CROD Element4-5MD Nastran Element Library3-22The Nastran Input File3-19Patran-Nastran Workflow and Files3-3Patran GUI2-48FEM References2-22Key Concepts in FEM2-7What is the Finite Element Method?2-3Engineering Methods1-32Company Information1-12Case Study: Landing Gear Strut1-9What is Patran?1-4What is MD Nastran?1-3Course Objectives Case Study: Stadium Arched Roof Truss4.0Basics of MD Nastran and Patran3.0Introduction to the Finite Element Method2.0Overview1.0PageSection  4Copyright  2008 MSC.Software Corporation CONTENTS 5-109Workshop 8 A-C “Tension Coupon”7-105Element Distortion6-82Workshop 7 “Tapered Plate”5-153Workshop 6 “Bridge Truss”5-59Workshop 5 “Coordinate Systems”7-52Loads7-45Single Point Constraints7-292-D Elements7-19Meshing6-76Post Processing CBEAM Results6-50Fields6-31The CBEAM Element6-19Material Properties5-149Post Processing CBAR Results5-142Multiple Subcases5-68The CBAR Element5-48Grid Points5-34Coordinate Systems5-3Introduction to Geometry Case Study: Aircraft Wing Rib7.0Case Study: Traffic Signal Pole6.0Space Station Truss5.0PageSection
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