Aerospace Structural Analysis Engineer

Course Name : Aerospace Structural Analysis Engineer  Course Code : QP AAS Q3103 Analyst Course Duration : 270 HrsCourse Start Date : 5th April 2021Course End Date : 7th Jun 2021Course 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 […]

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Course Overview

Course Name : Aerospace Structural Analysis
Course Code : QP
AAS Q3103 Analyst 
Course Duration : 270
Course Start
Date :
 5th April
Course End Date
 7th Jun 2021
Course Description :

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

  • Aircraft basics and
  • 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 :

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
  • 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
  3. Aircraft Electrical
  4. Aircraft Avionics
  5. Aircraft Propulsion
  6. Environmental Control
  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
  13. Failure theories
  14. Bending and deflection
    of beams
  15. SFD and BMD diagrams
  16. Aerospace metallic
  17. Aerospace Composite
  18. Composite
  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
  28. Basics of Crack
  29. Design Philosophies
  30. F&DT evaluation
  31. Service Repair Manuals-
  32. Concession – Overview
  33. Aircraft Repair
    Justifications – Overview
  34. Hand Calculation and
  35. Fastener stiffness
  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
  47. 2D Meshing complex components
  48. 2D Meshing assemble
    components, fasteners, and attachment
  49. 3D Meshing simple
  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

Mechanical/Aeronautical/Automobile Engineer or Engineering Students
Training Method: Instruction
Based Online Training & Virtual Classroom

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