FEM-Analysis---Helicopter-s-Tail

university-project

The purpose is to present a consistent finite-element formulation, developed to predict the free vibration characteristics of two different helicopters tailboom structures

How to download and setup FEM-Analysis---Helicopter-s-Tail

Open terminal and run command

git clone https://github.com/frank1789/FEM-Analysis---Helicopter-s-Tail.git

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it supports a few different network protocols and corresponding URL formats.

Also you may download zip file with FEM-Analysis---Helicopter-s-Tail https://github.com/frank1789/FEM-Analysis---Helicopter-s-Tail/archive/master.zip

Or simply clone FEM-Analysis---Helicopter-s-Tail with SSH

[email protected]:frank1789/FEM-Analysis---Helicopter-s-Tail.git

If you have some problems with FEM-Analysis---Helicopter-s-Tail

You may open issue on FEM-Analysis---Helicopter-s-Tail support forum (system) here: https://github.com/frank1789/FEM-Analysis---Helicopter-s-Tail/issues

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