
- •Общая постановка задачи
- •Исходные данные
- •Построение геометрической модели.
- •Определение прогиба крыши от собственного веса.
- •Модальный анализ
- •Гармонический анализ
- •Анализ и расчет измененной модели
- •Определение прогиба новой модели крыши от собственного веса
- •Модальный анализ
- •Гармонический анализ
- •Построение геометрической модели стеклопластиковой крыши
- •Модальный анализ
- •Гармонический анализ
Построение геометрической модели стеклопластиковой крыши
/prep7 Выбор типа элемента и задание характеристик материала et,1,shell99 mp,ex,1,24.6e9 mp,ey,1,18.6e9 mp,gxy,1,5e9 mp,prxy,1,0.012 mp,nuxy,1,0.3 mp,dens,1,2200 r,1,26,0,0,0,0,0 Rmore,0,0,0,0,0,0 rmore,1,0,0.00025,1,30,0.00025 rmore,1,60,0.00025,1,-60,0.00025 rmore,1,-30,0.00025,1,0,0.00025 rmore,1,-60,0.00025,1,60,0.00025 rmore,1,-30,0.00025,1,0,0.00025 rmore,1,-30,0.00025,1,0,0.00025 rmore,1,-30,0.00025,1,0,0.00025 rmore,1,-60,0.00025,1,60,0.00025 rmore,1,-30,0.00025,1,0,0.00025 rmore,1,-30,0.00025,1,0,0.00025 rmore,1,-60,0.00025,1,60,0.00025 rmore,1,-30,0.00025,1,0,0.00025 rmore,1,-30,0.00025,1,0,0.00025 Построение геометрической модели k,1,-0.3,0 k,2 k,3,0,-0.3 k,4,2.4,-0.3 k,5,2.4,0 k,6,2.7,0 k,7,2.7,1 k,8,2.4,1 k,9,2.4,1.3 k,10,0,1.3 k,11,0,1 k,12,-0.3,1 l,3,4 l,6,7 l,9,10 l,12,1 larc,1,3,2,0.3 larc,4,6,5,0.3 larc,7,9,8,0.3 larc,10,12,11,0.3 k,13,-0.3,0,0.1 k,14,0,0,0.1 k,15,0,-0.3,0.1 k,16,2.4,-0.3,0.1 k,17,2.4,0,0.1 k,18,2.7,0,0.1 k,19,2.7,1,0.1
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k,20,2.4,1,0.1 k,21,2.4,1.3,0.1 k,22,0,1.3,0.1 k,23,0,1,0.1 k,24,-0.3,1,0.1 l,3,15 adrag,5,1,6,2,7,3,9 adrag,8,4, , , , ,9 k,40, , ,0.4 larc,26,40,14,0.3 larc,25,40,14,0.3 adrag,28, , , , , ,13 arotat,28, , , , , ,14,40,-90 arotat,30, , , , , ,5,36,90 adrag,35, , , , , ,17 adrag,33, , , , , ,26 arotat,37, , , , , ,8,41,90 adrag,43, , , , , ,21 arotat,45, , , , , ,11,23,90 a,36,40,46,41 k,51,0.05,-0.3 k,52,0.14,-0.3 k,53,0.05,-0.3,-0.12 k,54,0.14,-0.3,-0.12 a,51,52,54,53 k,55,2.35,-0.3 k,56,2.26,-0.3 k,57,2.35,-0.3,-0.12 k,58,2.26,-0.3,-0.12 a,55,56,58,57 k,63,0.05,1.3 k,64,0.14,1.3 k,65,0.05,1.3,-0.12 k,66,0.14,1.3,-0.12 a,63,64,66,65 k,67,2.35,1.3 k,68,2.26,1.3 k,69,2.35,1.3,-0.12 k,70,2.26,1.3,-0.12 a,67,68,70,69 k,200,1.155,-0.3 k,201,1.245,-0.3 k,202,1.155,-0.3,-0.12 k,203,1.245,-0.3,-0.12 a,200,201,203,202 k,210,1.155,1.3 k,211,1.245,1.3 k,212,1.155,1.3,-0.12 k,213,1.245,1.3,-0.12 a,210,211,213,212 k,75,0.095,-0.3,-0.06 k,76,2.305,-0.3,-0.06 k,214,1.2,-0.3,-0.06 k,77,0.095,1.3,-0.06 |
k,78,2.305,1.3,-0.06 k,215,1.2,1.3,-0.06 circle,75,0.03,77 circle,76,0.03,78 circle,77,0.03,75 circle,78,0.03,76 circle,214,0.03,215 circle,215,0.03,214 al,79,80,81,82 al,75,76,77,78 al,91,92,93,94 al,87,88,89,90 al,95,96,97,98 al,83,84,85,86 asba,18,25 asba,22,26 asba,19,24 asba,20,29 asba,23,28 asba,21,27 aglue,all Разбиение полученной модели на конечно-элементную сеть smrtsize,1 mshape,0,2d amesh,all Исключение возможных перемещений кронштейнов по трем координатным осям dl,79, ,ux,0 dl,79, ,uy,0 dl,79, ,uz,0 dl,80, ,ux,0 dl,80, ,uy,0 dl,80, ,uz,0 dl,81, ,ux,0 dl,81, ,uy,0 dl,81, ,uz,0 dl,82, ,ux,0 dl,82, ,uy,0 dl,82, ,uz,0 dl,75, ,ux,0 dl,75, ,uy,0 dl,75, ,uz,0 dl,76, ,ux,0 dl,76, ,uy,0 dl,76, ,uz,0 dl,77, ,ux,0 dl,77, ,uy,0
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dl,77, ,uz,0 dl,78, ,ux,0 dl,78, ,uy,0 dl,78, ,uz,0 dl,67, ,ux,0 dl,67, ,uy,0 dl,67, ,uz,0 dl,68, ,ux,0 dl,68, ,uy,0 dl,68, ,uz,0 dl,69, ,ux,0 dl,69, ,uy,0 dl,69, ,uz,0 dl,70, ,ux,0 dl,70, ,uy,0 dl,70, ,uz,0 dl,71, ,ux,0 dl,71, ,uy,0 dl,71, ,uz,0 dl,72, ,ux,0 dl,72, ,uy,0 dl,72, ,uz,0 dl,73, ,ux,0 dl,73, ,uy,0 dl,73, ,uz,0 dl,74, ,ux,0 dl,74, ,uy,0 dl,74, ,uz,0 Задание узловых сил f,all,fz,-0.1 |
Приложение 2