Advance FE Analysis on Control Parameter

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Course Overview

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

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