mechanics-of-solids

There are 12 repositories under mechanics-of-solids topic.

  • jeevanjyoti4/advmechsolids

    Files for the course "Advanced Mechanics of Solids" in the Mechanical Engineering department of IIT Kharagpur

    Language:Jupyter Notebook14104

  • avgcampos/myfempy

    Myfempy is a python package based on finite element method to multiphysics analysis.

    Language:Python7140

  • bettachini/MecanicaAnaliticaComputacional

    Repositorio de la asignatura "Mecánica Analítica Computacional" de la carrera de grado en ingeniería mecánica de la Universidad Nacional de La Matanza.

    Language:Jupyter Notebook5403

  • adtzlr/cubrium

    cubrium - a cube in equilibrium

    Language:Python2402

  • emefff/Geometry-Generation-in-Salome-for-Composite-and-Porous-Materials

    Python scripting in Salome allows us to automatically generate random particles or pores. With subsequent operations we are able to build composite or porous bodies for study in Code_Aster.

    Language:Python2100

  • deepwithin/three-one

    Numerical problems of Heat Transfer and Adv. Mechanics of Solids using MATLAB

    1100

  • LuisCarlosRojasTorres/ViscoQT

    A program for linear viscoelastic material modeling

    Language:C++1100

  • alvin-biyoghe/stress-strain-hysterisis

    The following code is a simulation of a few stress-strain loops of a simple elasto-plastic material. The stress value is oscillated with with different amplitudes. The aim is to evaluate the dissipation between the loading and unloading phases, as well as the stress amplitude dependency of said dissipation.

    Language:Jupyter Notebook0210

  • charbileigh/Aircraft-Load-Distribution

    Background info of the program: This code is created to open a CSV file, then create a matrix of our distances. Then it is bound to go to an extent where it uses the Gaussian elimination method to get the inverse and then multiplying that with the necessary matrix to get the distributed load. Then from there, it needs to integrate the function to get coefficients for the shear and the bending moment, then get the constants, and then this code is going to allow us to know the bending moment of an aircraft wing. furthermore, we will create an output CSV file. From this, we can deduce the mechanical stresses using the correct equation.

    Language:Python0100

  • CraZMe/2BarG

    2BarG – A program to process split Hopkinson (Kolsky) bar test results

    Language:Python0101

  • CraZMe/2BarG_V1

    2BarG – A program to process split Hopkinson (Kolsky) bar test results

    Language:Python0101

  • hennessymatt/UnconfinedCompression

    Simulates the unconfined compression of nonlinear poroelastic materials

    Language:Python0100