ჩარიცხვის პარამეტრები
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