Aerospace Structural Analysis Engineer Batch – 3

Course Name : Aerospace Structural Analysis Engineer  Batch – 3 Course Code : B305ASA Analyst Course Duration : 270 Hrs Course Start Date : 10th August 2021 Course End Date : 12th October2021 Course Description : In this course the learners will get insight about the below topics. Aircraft basics and systems Aircraft Structure Metallic and Non-Metallic Materials GFEM and DFEM / Selection of elements (FEM/FEA) Fatigue […]

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Course Overview

Course Name : Aerospace Structural Analysis Engineer  Batch – 3

Course Code : B305ASA Analyst

Course Duration : 270 Hrs

Course Start Date : 10th August 2021

Course End Date : 12th October2021

Course Description :

In this course the learners will get insight about the below topics.

  • Aircraft basics and systems
  • Aircraft Structure
  • Metallic and Non-Metallic Materials
  • GFEM and DFEM / Selection of elements (FEM/FEA)
  • Fatigue and Damage Tolerance of metallic Materials
  • Hand Calculation and Allied Topics (SRM/Repair/Concession)
  • Hypermesh -FEM
  • Analysis -FEA

Course Outcome :

By end of this course learners will be able

  • To perform airframe structural design validation through hand calculations and finite element analysis for every primary and secondary structures like wings skin and attachment joints and brackets.
  • To understand loads and load path in structures, thus, can create very good quality finite element model with appropriate loading and boundary conditions
  • To perform stress analysis activities related to aircraft structural modifications, role change, upgradation, certification, and customization.
  • To perform concessions, repair and SRM justification activities.
  • To perform the design validation of aircraft interiors, brackets, and other secondary structural members
  • To perform structural analysis activities related to design optimization, design modification, weight reduction, reverse engineering tasks.
  • Can interpret and comment logically on the sufficiency, validity, and correctness of the finite element analysis results

Course Content:

  1. Aircraft Basics
  2. Aircraft Mechanical Systems
  3. Aircraft Electrical Systems
  4. Aircraft Avionics System
  5. Aircraft Propulsion Systems
  6. Environmental Control Systems
  7. Aircraft Interior
  8. Human Factor
  9. Fundamental of Design
  10. Loads, stress strain, Stress Strain Curves
  11. Determinate and indeterminate structures
  12. Principal stress and strain
  13. Failure theories
  14. Bending and deflection of beams
  15. SFD and BMD diagrams
  16. Aerospace metallic materials
  17. Aerospace Composite materials
  18. Composite Manufacturing
  19. Composite Machining Inspection and QC
  20. Basics of Finite Element Analysis
  21. Engineering Problem Solving techniques
  22. Selection of elements, Element order and accuracy control
  23. Meshing Guidelines, validation techniques
  24. GFEM and DFEM Requirements and Handling
  25. MSC-Nastran Overview
  26. Basics of Fatigue
  27. Basics of Fracture Mechanics
  28. Basics of Crack Propagation
  29. Design Philosophies
  30. F&DT evaluation
  31. Service Repair Manuals- Overview
  32. Concession – Overview
  33. Aircraft Repair Justifications – Overview
  34. Hand Calculation and application
  35. Fastener stiffness calculations
  36. Introduction to Hypermesh GUI
  37. Understand the Hypermesh options and capabilities
  38. Getting started with Hypermesh geometry, software compatibility
  39. Geometry creation / handling / editing
  40. Hypermesh Geometry Import Export and geometry cleanup
  41. Geometry preparation for FE Mesh / defeaturing and editing
  42. Getting ready geometry for FE Mesh, options, and parameters settings
  43. HM Meshing parameters control and settings
  44. Auto meshing, mesh modification & HM short cut keys
  45. 1D and 2D Meshing
  46. 2D Meshing medium components
  47. 2D Meshing complex components
  48. 2D Meshing assemble components, fasteners, and attachment
  49. 3D Meshing simple components
  50. 3D Meshing medium and complex components, use of higher order elements
  51. PATRAN GUI, Model creation and import to solution deck
  52. Free-free / Normal mode and Linear static analysis Post Processing and result interpretations
  53. Types of non-linearity and preparing for non-Linear analysis, Buckling / dynamic / frequency response analysis

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer or Engineering Students

Training Method: Instruction Based Online Training & Virtual Classroom

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