Analysis

Course Name : Aerospace Structural Analysis Engineer  Batch - 3

Course Code : B305ASA Analyst

Course Duration : 270 Hrs

Course Start Date : 14^th Dec 2023

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

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

Course Name : Aerospace Structural Analysis Engineer  Batch - 3

Course Code : B305ASA Analyst

Course Duration : 270 Hrs

Course Start Date : 14^th Dec 2023

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

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

Course Name : Aerospace Structural Analysis Engineer  Batch - 3

Course Code : B305ASA Analyst

Course Duration : 270 Hrs

Course Start Date : 14^th Dec 2023

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

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

Course Name : Aerospace Structural Analysis Engineer  Batch - 3

Course Code : B305ASA Analyst

Course Duration : 270 Hrs

Course Start Date : 14^th Dec 2023

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

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

Course Name : Aerospace Structural Analysis Engineer  Batch - 3

Course Code : B305ASA Analyst

Course Duration : 270 Hrs

Course Start Date : 10^th August 2021

Course End Date : 12^th 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

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

Course Name : Aerospace Structural Analysis Engineer  Batch - 2

Course Code : B205ASA Analyst 

Course Duration : 270 Hrs

Course Start Date : 24^th May 2021

Course End Date : 7^th Jun 2021

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

Course Name: Free Course on Aerospace Analysis

Course code : AE21A001

Course Duration : 5 hours

Course description:

Hello, everyone, welcome to this introductory course on Aircraft Basics and classical hand calculation from BridgeNow Academy.

Key pointers about the course are given below.  

·       Major aircraft structural components and their functions and role

·       Classification of aircraft and aircraft structural components

·       Requirements for aerospace materials

·       Classifications of metallic and composite structural materials

·       Relative advantages and disadvantages of aerospace materials

·       Application and significance of hand calculations

·       Hand calculations as engineering problem solving techniques

·       Why knowing hand calculation is important for design engineers

·       Hand calculations as design validation and as standalone design tool

·       Various engineering problem solution using hand calculations

·       Comparison between hand calculations and other numerical methods

·       Advantage and disadvantages of classical hand calculations?

·       Best practices in performing hand calculations

Course Takeaways / Overview

·       Major aircraft components, their functions and classification

·       Design and fundamental required properties of aerospace materials

·       Comparison of metallic and composite materials

·       Classification of metallic and composite materials

·       Classical hand calculation and its importance as design tool

·        Seven step method to solve the engineering problems

·        Why engineers should know classical way of calculation

·        How hand calculations can be used as standalone design tool and also as a design validation and optimization tool.

·        Free body diagrams and design of brackets, riveted joint, bolted, lug joints

·       Best practices in classical method of calculations

Course Structure:

·       Lesson 1: Main parts of aircraft

·       Lesson 2: Aircraft Materials (metallic)

·       Lesson 3: Aircraft Material (Composites)

·       Lesson 3: Classical Hand Calculations

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based

Course Validity: 5 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

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

Course Name: Fundamentals of Design

Course Code:  AE20AM2001V0

Course Description:

·       Importance of units and dimensions in engineering projects

·       Design and design processes in engineering

·       Types of designs

·       Design considerations for successful product development

·       Repercussions of poor design

·       Common mistakes during design

·       Common misconceptions during product design

·       Engineering product life cycles

·       Best practices during product design

 Course Overview

·       Units fundamentals

·       Choice and selection of unit system

·       Design and design processes in engineering

·       Design considerations for product development

·       Repercussion of poor design

·       Common mistakes during design

·       General misconceptions during product design

·       Engineering product life cycle

Course Structure:

·       Lesson 1: Fundamentals of Design

·       Lesson 2: Loads, stress strain, Stress Strain Curves

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based.

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

Course Name: Solid Mechanics I

Solid Mechanics I - AE20AM2002V0

Course Description:

·       Solid mechanics is the study of the deformation and motion of solid materials under the action of forces.

·       Determinate, indeterminate beam problem solution

·       Applications and limitations of determinate and indeterminate beams

·       Integration method, Moment area and conjugate beam method to solve indeterminate beams for deflection and slopes

·       Principal stress and strain – Analytical and graphical method (Mohr circle)

·       Various failures, their types, causes and  consequences.

·       Application and details of failure theories for ductile and brittle materials

·       Engineering applications of slid mechanics concept in engineering design

Course Overview

·       Concept of load, stress and strain

·       Classification of failure, their causes and consequences

·       Failure theories for ductile and brittle materials

·       Deflection and slope of determinate and indeterminate beams

·       Method of integration, moment area and conjugate beam method

·       Concept of principal stress and strain, principal planes and application for failure prediction

·       Best practice for application of solid mechanics concept for product design

Course Structure:

·       Lesson 1: L1_Determinate and indeterminate structures

·       Lesson 2: L1 - Principal stress and strain

·       Lesson 3: L1 - Failure theories

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based.

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

Course Name: Basics of Solid Mechanics Level II

Course Code: AE20AM2003V0

Course Description:

·       Solid mechanics is the study of the deformation and motion of solid materials under the action of forces.

·       Flexural equations and its application for the solution for indeterminate beam problems.

·       Slope and deflection of standard and nonstandard beams using method of integration and moment area method

·       Shear force and bending moment diagrams are analytical tools used in conjunction with structural analysis to help perform structural design by determining the value of shear force and bending moment at a given point of a structural element such as a beam

·       These diagrams give designer an overview of the result for the combination of different forces and their likely implications on the structure, and its stability

·        It helps to decide the constructional constraints, which should be taken care of while designing

·       It helps to understand the failure of a beam under combined loading, where we can see that, both bending moment and shear force plays an important role in its failure as compared to tension and compression alone

·       Thus, it is important to find out their variation along the length of the beam using shear force and bending moment diagrams.

Course Overview

·       Deflection and slope determination using integration method and moment area method

·       Advantages and limitations of determinate and indeterminate beams

·       Solution of determinate and indeterminate beam problems

·       Shear force and bending moment calculations for simple and complex loading

·       Application of shear force and bending moment diagram as design aid

·       Effect of eccentric force on attached parts

·       Best practices in SF and BM estimation

·       Determination of point of contraflexure and location of maximum shear force

Course Structure:

1.       Bending and deflection of beams

·       Lesson 1: Bending and deflection of determinate beams

·       Lesson 2: Bending and deflection of Indeterminate beams

2.       SFD and BMD diagrams

·       Lesson 1: Shear force and bending moment - introduction

·       Lesson 2: Simple examples SFD and BMD

·       Lesson 3: Advance examples SFD and BMD

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based.

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

Course Name: Aircraft Materials

Course Code : AE20AM3001V0

Course Description:

In this course on aircraft metallic materials from BridgeNow Academy.

Key pointers about the course on aircraft metallic materials

·       Recommended properties of aircraft structural materials

·       List of metallic materials used in aircraft industry

·       Classification of metallic materials

·       Ferrous and non-ferrous metals and alloys

·       Alloying and heat treatment processes, effect of alloying materials

·       Relative advantages and limitations of metallic materials

·       Reasons for selection of metallic materials as structural material

·       Metallic material components used in commercial aircraft

·       Recommended properties of aircraft structural materials

·       Advantages of composite materials used in aircraft industry

·       Classification and nomenclature of composite materials

·       Composite material parameters controlling the mechanical properties

·       Relative advantages and limitations of composite materials

·       Reasons for selection of composites as structural material

·       Why composite materials are so popular as structural material?

·       Composite material components used in commercial aircraft

Course Takeaways / Overview

·       Performance requirements of aircraft structural materials

·       Metallic materials used in industry and their classification

·       Relative advantages and disadvantage of metallic materials

·       Metallic materials and composite materials which one is a better choice?

·       Alloying materials and their effect on material properties

·       Heat treatment processes and their effect on material properties

·       Metallic materials application and their classification

·       Performance requirements of aircraft structural materials

·       Composite materials used in industry and their classification

·       Relative advantages and disadvantage composite materials

·       Metallic materials and composite materials which one is a better choice?

·       Composite materials application and their classification and nomenclature

Course Structure:

Lesson 1: Aircraft Metallic Materials

Lesson 2: Aircraft Composite Materials 

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based.

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

Course Name: Composite Material Industry

Course Code:  AE20AM3003V0

Course Description:

In this course on composite material Industry under aircraft materials from BridgeNow Academy.

Key pointers about the course on aircraft metallic materials

·       Requirements for selection of manufacturing process

·       Goals of a composite manufacturing method

·       Objectives of a composite machining operations

·       Objectives of a composite inspection and quality control

·       Manufacturing parameters

·       Different manufacturing methods and selection of manufacturing method

·       Relative advantages and disadvantages of different composite manufacturing methods

·       Automation requirements and challenges

·       Composite defects, inspection methods and quality control

·       Different machining operations and selection of machining process

·       Bonding of composite materials an alternative to creating joint

·       Relative advantages and disadvantages of different machining operations

·       Different inspection methods and selection of inspection method for quality control

·       Best practices in composite machining, inspection, and quality control

·       Best practices in composite manufacturing, machining and quality control

Course Takeaways / Overview

·       Selection of manufacturing, machining and inspection methods

·       Various composite manufacturing, machining and inspection methods

·       Relative advantages and disadvantages of various composite manufacturing, machining and inspection methods

·       Automation requirements and challenges for composite manufacturing

·       Best practices in composite manufacturing, machining, inspection and quality control

Course Structure:

·       Lesson 1: Lesson 1: Composite Manufacturing

·       Lesson 2: Composite Machining inspection and Quality control

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based.

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

Course Name: Basics of Finite Element Analysis

Course Code : AE20AM4001V0

Course Description:

In this course on basic FEM are given below. In these lessons,  following questions will be addressed on basic FEM that, what is/are:

·       Knowing FEM means and its importance

·       Significance of equilibrium of system

·       Degree of freedom

·       Infinite and finite degree of freedom problems

·       Exact and approximate solution

·       Convergent and divergent solutions

·       FEM and other numerical methods of solutions

·       Meshing guidelines for FE model creation

·       Element selection criteria

·       FEM is an approximate solution means

·       Accuracy of FEM solution

·       Validation and verification of FEM results

Course Takeaways / Overview

·       Industries using FEM for design and development

·       FE meshing and meshing guideline

·       Best practice for FE mesh creation

·       Simplifications in FEA and its effect on FEA results

·       limitations of FEA

·       Element selection and higher order element

·       Element stiffness matrix

·       Accuracy control of FE analysis

·       Validation and verification techniques of FEA results

·       GFEM and DFEM requirements

Course Structure:

·       Lesson 1: Basics of Finite Element Analysis

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based.

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

Course Name: NASTRAN Fundamentals

Course Code: AE20AM4003V0

Course Description

In this course on Nastran Fundamentals from BridgeNow Academy.

Key pointers about the course on MASC Nastran overview are given below. In these lessons,  following questions will be addressed on NSC Nastran fundamentals, what is/are:

·       Role of solver in Finite element analysis

·       NASTRAN and its role

·       NASTRAN formulation and FORTRAN code

·       FORTRAN Modules control and Direct Matrix Abstraction Program (DMAP)

·       NASTRAN solution sequence for analysis type

·       NASTRAN file structure and NASTRAN statements

·       NASTRAN as solver for PATRAN, Hypermesh, MARK etc.

·       NASTRAN input and output files and output control

·       Handling big database and use of include files

·       NASTRAN cards and execution control statements

·       Library of Finite Elements in NASTRAN

Course Takeaways / Overview

·       How to use NASTRAN as solver

·       With which pre-processors NASTRAN is compatible

·       NASTRAN control cards and execution control

·       NASTRAN file structure and NASTRAN statements

·       NASTRAN input and output files and output control

·       NASTRAN element and material libraries

Course Structure:

·       Lesson 1: L1_NASTRNA Fundamentals

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based.

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

Course name: Introduction to Fatigue

Course Code: AE20AM5001V0

Course Duration: 6 hrs.

Course Description:

In this course on introduction to fatigue from BridgeNow Academy. This course contains four lessons covering following takeaways. 

Course Overview:

Understand the overview of fatigue 

Understand the overview of S-N curve

Learn about the parameters that affect endurance limit and fatigue strength of material

Know about the effect of mean stress and notch on fatigue life

Understand the overview of constant amplitude loading

Know about the Miner’s rule of linear damage summation rule

Understand the overview of variable amplitude loading

Know about different types of cycle counting technique

Course Structure:

Lesson 1: Introduction to fatigue

Lesson 2: S-N curve

Lesson 3: Fatigue life under constant amplitude loading

Lesson 4: Fatigue life under variable amplitude loading

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA

Course Name: Introduction to Fracture Mechanics

Course Code: AE20AM5002V0

Course Duration: 5 hrs.

Course Description:

In this course on introduction to fracture mechanics from BridgeNow Academy. This course contains four lessons covering following takeaways. 

Course Overview:

Overview of fracture mechanics

Understand the stress intensity factor

Learn about the crack tip plasticity

Know the relationship between defect size, loading and fracture toughness

Understand the effect of thickness and orientation on fracture toughness

Know the procedure to determine plane strain fracture toughness through testingCourse Structure:

Lesson 1: Introduction to fracture mechanics

Lesson 2: Stress intensity factor

Lesson 3: Fracture toughness

Lesson 4: Plane strain fracture toughness testing

Pre-requisite:   Mechanical/Aeronautical/Automobile Engineer

Training Method: Instruction based

Course Validity: 90 days from the date of enrolment.

Downloadable Exercises: NA

Recommended Practice Hours: NA