Example |

Input: |

Length of plate in x-axis direction a: |
1 |

Length of plate in y-axis direction b: |
0.5 |

Elasticity modulus in x-axis direction E_{x}: |
10000 |

Elasticity modulus in y-axis direction E_{y}: |
1000 |

Poisson's ratio of the material ν_{yx}: |
0.03 |

Shear modulus of the material G: |
385 |

Plate thickness h: |
0.01 |

Uniform load q: |
0.00278 |

Coordinate x of point A of load area x_{0}: |
0.205 |

Coordinate y of point A of load area y_{0}: |
0.105 |

Length of load area in x-axis direction l_{x}: |
0.102 |

Length of load area in y-axis direction l_{y}: |
0.052 |

Output: |

Maximum normal stress in x-axis direction is 0.35657236 at x=0.25 and y=0.1375

Corrresponding stresses are: σ

Maximum normal stress in y-axis direction is 0.12005951 at x=0.2625 and y=0.13125

Corrresponding stresses are: σ

Maximum shear stress in x-axis or y-axis direction is 0.04187217 at x=0.0 and y=0.0

Corrresponding stresses are: σ

Maximum principal stress is 0.35675135 at x=0.25 and y=0.1375

Corrresponding stresses are: σ

Maximum shear stress is 0.12066183 at x=0.25 and y=0.15

Corrresponding stresses are: σ

Maximum von Mises stress is 0.3148587 at x=0.25 and y=0.1375

Corrresponding stresses are: σ