Course Name: FE Analysis control parameter- Advance

Course Code: AE20AM8003V0
 

Course Description :

In this course on analysis tool training
advance and basic, from BridgeNow Academy.

Key pointers about the course on aircraft metallic
materials

·       Creation of advanced FE model in another pre-processor like PATRAN
or use of FE model created in Hypermesh into another pre-processor by importing
HM files.

·       Update and modify properties, materials, loads and boundary
conditions etc. Isotropic, anisotropic and orthotopic material creation like
Metallic and composite.

·       Use of utility and tool bar menu options for advance meshing and
analyses.

·       Example problem from MSC software for common non-linear static
analysis, buckling and post buckling analyses, frequency response and shock
load analyses.

·       Application of knowledge base from example problem to a real complex
engineering problem for above analyses.

·       Creation of analysis deck for non-linear static analysis, buckling
and post buckling analyses, frequency response and shock load analyses.

·       Analysis control parameters for advance analyses and submission of
analysis deck to solver.

·      
Perform post process of the analysis
results and result interpretation.

Course Takeaways / Overview

The takeaways from this course are

·       Importing and update advance FE model created in Hypermesh into
other pre-processors.

·       Element properties and respective metallic and composited material
applied to FE model.

·       To create and edit the solver deck outside pre-processor for
advanced analyses

·       Application and use of utility and tools option for advance meshing

·       Advanced example problem and extrapolation of knowledge to real
complex engineering problems

·       Solution parameter control for non-linear, buckling and post
buckling analyses, frequency response and shock and impact analyses

·       To import, visualize and interpret the FEA results

·      
To make logical conclusions
from analysis results and result presentation

 Course Structure:

·       Lesson 1: Types of non-linearity and preparing
for non-Linear analysis

·       Lesson 2: Buckling and post buckling Analysis

·       Lesson 3: Direct Transient & dynamic shock
load analysis

·       Lesson 4: Frequency response 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