PROGRAMS CONCERNING MECHANICS IN FORTRAN 90


Choose a source program (*.F90) by clicking the appropriate button.

BEAM.F90
CIRCUIT.F90
1DOF01.F90
1DOF02.F90
MODES.F90
NDOF01.F90
NDOF02.F90
NDOF03.F90
NDOF04.F90
BEAM1.F90
PENDULUM.F90
COMPOS01.F90
COMPOS03.F90
COMPOS04.F90
Program Description

  • Calculate beam deflection for four different support/loading systems
  • Use Runge-Kutta method to solve a LRC circuit or equivalent damped mass-spring problem
  • Response of a 1 dof Mass-Spring System with damping to a sinusoidal input force
  • Response of a 1dof Mass-Spring System with viscous damping to a periodic input force: M X" + C X' + K X = F(t)
  • Frequencies and Modes of Mass-spring Systems without Damping By Transfer Method
  • Response of a N d.o.f. Mass-Spring System with Damping to a sinusoidal Force By Transfer Matrices Method
  • Frequencies and eigenmodes, masses and modal stiffnesses of a Mass-Spring undamped system represented by Motion Equation: [M] . [X]" + [K] . [X] = [0].
  • Response of a N d.o.f. Mass-Spring System with Damping to a sinusoidal Force By a Direct Method
  • Step by step solution of system [M] X" + [C] X' + [K] X = F(t) By the "Wilson-Theta" Method
  • Resonance Frequencies of a bending beam, Modal Mass and Stiffness, Deformation modes and Maximum Strain
  • Calculate angular motion of an elementary Mass Pendulum NEW
  • Calculate the stresses in a unidirectional layer of a composite material, knowing deformations exx, eyy, gxy, and angle theta of fibers in x direction NEW
  • Calculate the matrix linking the stresses to deformamations in a laminated material made of n unidirectional composite layers NEW
  • Calculate the deformations and stresses in a laminated material made of n unidirectional composite layers, knowing the resulting imposed efforts NEW


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© J-P Moreau Last modified 06/15/2006 - E-mail: jpmoreau@wanadoo.fr