施威德勒型球面网壳的建模过程详解

施威德勒型球面网壳的建模过程详解1、问题描述：一球面半径20.0m，跨度35m，矢跨比1:3.5的单层球面网壳。网桥结构所有杆件均采用Φ114.0×4.0的Φ235钢管。建模过程中所有数据单位统一为N-mm制。模型侧视图模型俯视图模型轴测图2、此问题拟采用ANSYS建模和受力分析。3、施威德勒型球面网壳建模及分析命令流。!结构建模finish/clear/filename,schwedler/title,analysisofsphericalreticulated-shell/prep7et,1,beam4r,1,1382,2093500,2093500,114,114,,rmore,,4187000,,,,,mp,dens,1,7.85e-9mp,ex,1,2.06e5mp,nuxy,1,0.3local,11,2,0,0,0cscir,11,1n,1,20000,0,30n,10,20000,180,30n,18,20000,340,30fill,1,10fill,10,18ngen,6,18,1,18,1,0,0,10n,109,20000,0,90*do,i,1,91,18e,i,i+1egen,17,1,i,i,1e,i+17,i*enddoe,1,19egen,5,18,109,109,1egen,18,1,109,113,1*do,i,91,108,1e,i,109*enddo*do,i,1,73,18e,i,i+19*enddoegen,17,1,217,221,1*do,i,18,90,18e,i,i+1*enddocsys,0nsel,s,loc,z,9900,10100d,all,,,,,,ux,uy,uz,,!网壳结构的固有振动特性分析/solantype,modalmodopt,lanb,6modopt,lanb,6,0,0,,offsolvefinish/post1set,listset,firstpldisp,0anmode,10,0.5,,0set,nextpldisp,0anmode,10,0.5,,0set,nextpldisp,0anmode,10,0.5,,0set,nextpldisp,0anmode,10,0.5,,0set,nextpldisp,0anmode,10,0.5,,0set,nextpldisp,0anmode,10,0.5,,0finish！特征值屈曲分析nsel,allf,all,fz,-1.00/soluantype,0eqslv,sparpstres,onsolvefinish/soluantype,1bucopt,lanb,6,0,0maxpand,6,0,0,1,0.001,solvefinish/post1set,firstpldisp,2set,nextpldisp,2set,nextpldisp,2set,nextpldisp,2set,nextpldisp,2set,nextpldisp,2finish!考虑初始缺陷的非线性屈曲分析/prep7tb,biso,1,1,2,tbtemp,0tbdata,,2.0e8,0,,,,upgeom,35,1,1,schwedler,rst,finish/solantype,0nlgeom,1outres,all,allarclen,1,0,0,arctrm,u,100,109,uznsubst,200,,,1solvefinish/post26nsol,2,109,u,z,deflectionrforce,3,1,f,z,reactionf/axlab,x,deflection/axlab,y,reactionfxvar,2plvar,3Finish4、可视化后处理及分析结果显示。I:网壳结构的固有振动特性分析网壳的前六阶固有频率网壳结构的第一阶振动模态网壳结构的第二阶振动模态网壳结构的第三阶振动模态网壳结构的第四阶振动模态网壳结构的第五阶振动模态网壳的第六阶振动模态II：特征值屈曲分析注：屈曲分析分为三个步骤：首先是设置预应力选项并执行一次静力分析，然后计算屈曲模态，最后扩展屈曲模态。网壳结构的第一阶屈曲模态网壳结构的第二阶屈曲模态网壳结构的第三阶屈曲模态网壳结构的第四阶屈曲模态网壳结构的第五阶屈曲模态网壳结构的第六阶屈曲模态