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FEM-Course-Matlab/6.桁架结构matlab有限元编程/Truss2D/Result.txt

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init project
2024-01-28 16:46:36 +00:00
U 0.083733 0.016008 0.039661 0.026328 0.037175 -0.0085763 0.01822 0.021831 0.015148 0.005787 0.01562 -0.012252 0.0050295 0.013812 0.0042759 0.0087074 0.0030177 -0.0023908 0.0034667 -0.0092859 -2.1948e-15 2.4339e-15 1.517e-14 1.767e-14 9.4811e-15 -1.1574e-14
Stress 76.3879 -34.7226 -8.69847 69.1407 7.24676 7.24754 -41.9695 -10.7523 1.65225 60.183 8.95432 17.5857 -3.09149 -1.37392 -40.5921 -2.63746 -4.40368 1.57158 59.0834 15.8718 2.16142 18.4816 -0.428496 -1.28658 -7.95028 -39.9367
AxialForce 229.1637 -104.1677 -26.09541 207.4221 21.74027 21.74261 -125.9085 -32.25681 4.956743 180.5489 26.86297 52.75716 -9.27447 -4.121749 -121.7764 -7.912368 -13.21104 4.714752 177.2501 47.61554 6.484248 55.44469 -1.285487 -3.859733 -23.85085 -119.8101
U 0.083733 0.016008 0.039659 0.026329 0.037175 -0.0085769 0.018218 0.021832 0.015146 0.0057873 0.015619 -0.012253 0.0050281 0.013813 0.0042744 0.0087079 0.0030162 -0.0023909 0.0034653 -0.009287 -2.2034e-15 2.4343e-15 1.5171e-14 1.767e-14 9.4835e-15 -1.1573e-14
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AxialForce 229.1667 -104.1667 -26.09053 207.4246 21.74211 21.74211 -125.9088 -32.25308 4.959728 180.547 26.87757 52.75278 -9.268564 -4.133107 -121.7757 -7.913732 -13.21101 4.716203 177.2496 47.60779 6.495102 55.46116 -1.297716 -3.870768 -23.84203 -119.8106
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Stress 76.3889 -34.7222 -8.69684 69.1415 7.24737 7.24737 -41.9696 -10.751 1.65324 60.1823 8.95919 17.5843 -3.08952 -1.3777 -40.5919 -2.63791 -4.40367 1.57207 59.0832 15.8693 2.16503 18.4871 -0.432572 -1.29026 -7.94734 -39.9369
AxialForce 229.1667 -104.1667 -26.09053 207.4246 21.74211 21.74211 -125.9088 -32.25308 4.959728 180.547 26.87757 52.75278 -9.268564 -4.133107 -121.7757 -7.913732 -13.21101 4.716203 177.2496 47.60779 6.495102 55.46116 -1.297716 -3.870768 -23.84203 -119.8106
U 0.40192 0.017967 0.18247 0.051274 0.18106 -0.03134 0.074859 0.045706 0.071613 0.0066397 0.07334 -0.035155 0.015777 0.028969 0.012076 0.015133 0.011461 -0.008209 0.014248 -0.024477 -1.1259e-14 2.8305e-15 4.1542e-14 3.3262e-14 3.3173e-14 -2.7525e-14
Stress 112.7334 -77.13337 -4.94935 105.6855 7.047878 7.047878 -84.18125 -11.361 6.046018 89.50744 16.17807 31.83548 -17.73972 -8.609533 -75.57171 -12.95458 -2.152677 9.754641 80.28377 33.2732 12.99948 24.40485 -9.001382 -9.788453 -24.44944 -68.6264
AxialForce 338.2001 -231.4001 -14.84805 317.0565 21.14363 21.14363 -252.5437 -34.083 18.13805 268.5223 48.53421 95.50644 -53.21917 -25.8286 -226.7151 -38.86374 -6.45803 29.26392 240.8513 99.81961 38.99845 73.21455 -27.00415 -29.36536 -73.34832 -205.8792
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AxialForce 338.2001 -231.4001 -14.84805 317.0565 21.14363 21.14363 -252.5437 -34.083 18.13805 268.5223 48.53421 95.50644 -53.21917 -25.8286 -226.7151 -38.86374 -6.45803 29.26392 240.8513 99.81961 38.99845 73.21455 -27.00415 -29.36536 -73.34832 -205.8792
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Stress 112.7334 -77.13337 -4.94935 105.6855 7.047878 7.047878 -84.18125 -11.361 6.046018 89.50744 16.17807 31.83548 -17.73972 -8.609533 -75.57171 -12.95458 -2.152677 9.754641 80.28377 33.2732 12.99948 24.40485 -9.001382 -9.788453 -24.44944 -68.6264
AxialForce 338.2001 -231.4001 -14.84805 317.0565 21.14363 21.14363 -252.5437 -34.083 18.13805 268.5223 48.53421 95.50644 -53.21917 -25.8286 -226.7151 -38.86374 -6.45803 29.26392 240.8513 99.81961 38.99845 73.21455 -27.00415 -29.36536 -73.34832 -205.8792
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Stress 112.7334 -77.13337 -4.94935 105.6855 7.047878 7.047878 -84.18125 -11.361 6.046018 89.50744 16.17807 31.83548 -17.73972 -8.609533 -75.57171 -12.95458 -2.152677 9.754641 80.28377 33.2732 12.99948 24.40485 -9.001382 -9.788453 -24.44944 -68.6264
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