ABAQUS复合材料教程

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详细的ABAQUS复合材料教程!详细的ABAQUS复合材料教程!
圆忘正七工Dt血贮 mesh M ai:nc4 Wat: To shang.Iep的8Tit4n》' mesh, you fus也tipt里面红 aAats-effrat Er an g har ins;anees 1.5 FX Step, Create Step: Proccdurc type=Static, Gcncral: Basic: Nlgcom=off Type static,所en旺 Basic Iacr enentati onother Tire period nesen ooff (ais, setting csatrals the inclusion of, monlinear effcts Automatie stabilization:wxne L Inelude adiabats heating effects ww.doci 哪E a 1.6 EN Load, Create Load: Step=Step-1 Mechanical=Concentrated force: CF1=1000 Nane ladl Ty;C哪t温 tea fore 江p Ra oa; Picked Edit Region. es8:Gel)区 dit.Create D atribution; Uniform 会〓童 leD 0 CRested □ Follow nodal rotat:an Wote- Force will be applied per aode. I Cancel 1.7 it Iz Boundary Condition Create Boundary Condition: Step=Step-1 MechanicalaDisplacement/Rotation: U1=0 U2=0 U3=0 URI=O UR2=0 UR3=0 当Madl idit Boundary Condition Step: Step-1 (Static, Geaeral Regi on: Picked) iElt legis . csIs:(GLobal)Edit.Erase. Distribution Uniforn Wvte:Tne山s2xeek 1.8建立Mesh, Mesh Type: Element Type=S8R 1.9 tiz Job, Create Job: Name=Job-I Model=Model-1: Submit ■del Type Status lrrt】 山Ayi:C9 aplied Crat吧 Reine=. belote[ Dismiss 1.10查看计算结果 Visualiz ation: Plot Contours on Deformed Shape: u Magtinude ⊙D10b-1, odF AFE山恋 dsrd62+Tot1220:20aaMT+1002010 formed ari U Deforroton scale Fatter中e,巧B牛02 2.采用 Solid element建立 Solid Composite Layups 2.1 E part-2, Creat Part: 3D Type=Deformable Shape=Solid Extrusion: Depth=0.8 (E: 这里的 Depth是 Composite Layup的总厚度) E山 t Fart fartI ModElINg Sp C 3n o2n Pl ansr O Axi symmetrie DEformablE O discrete rigid don+avaiLabLe 区 O Analytical rigid EUlerian +甘 22建立 Materia1, Mechanical: Elasticity: Elastic:Type= Engineering Constants在data中 输入材料参数:EI=25.0E6E2=10E6E3=10E6Nu12=025Nu13=025Nu23=025G12=05c6 G13=0.5E6G23=0.2E6 Edt ater工a⊥ Hame: Material-1 r Description Edit Mat些ia1Beha16s General Mechani cal Thermal ither Deletel Type: Engineering Constants v ≤ ubopti or 口s∈ temperature-dependent通ata Rumber o- fie1va1ah1画雪 Moduli time scale (for vi seoelastieity): Long-term □W。 compression o tens or Dat难 r量 Hu1- 10口 ≤ 0a 2.3 E. Composite Layup, Composite Layup Manager: Create: Initial ply count=4 Element Type= Conventional Shell生成4层的具体数据如下图所示(注:参数 Element Relative Thickness为相对于总厚度的比例,并不是实际厚度,其总和可以不为1) Eiit Composite Layn Element type: solic Description Layup Orientation Stacking Direction efinition: Coordinate systen ELement direction I Datas eays-1 Select . Crea; e. ○ Element direction2 B心tAis:OA1●Ai2⊙Ai3 ⊙ Element direction3 Additieaalrotation:OHone O Angle: o DIstribution: I 9飞吧 Plist Displa I I Bake calcul ated sections =ymmetric 喵|即|y El必酽量 Ply Bome Region aterialRelative Kata重 ntepratIOT Thian鲁服写 Ana⊥e Fly layups 45 2 v P12 固 teria1-1 Layup)-45 11y3 Ci cked Materlal-l told MatoriaL-l Caneal 2.4 E/X Instance, Create Instance: Parts=Part-1 Instance Type=Independent: OK x下2 Farts fart-1 O Dependent (n∈ sh on part ⊙工 ndependent fresh.,aans Hote: Ta chanze a Dependent instance s aNto-offsat fr on <ther instances 2.5 EJX Step, Create Step: Procedure type=Static, General: Basic: Nlgeom=off 2Mna:“F-1 icK amstat oorE M3OC“6=1t3 Autonatic stabilization Nons B sde adiabatic heating effects 2.6 E Load, Create Load: Step=Step-1 Mcchanical=Concentrated force: CF1=1000 L08f-1 Coneentrated force tep: 5to l stadie Genera) Regi sn: (Picked)E4: R+gi on cts: ictal)氐g司 Distribution! reform IC AmpLitude Cristea □F11 oy modl rotation 固t看,FT:置1b41: d par nsd 27建立 Boundary Condition Create Boundary Condition: Step=Step-1 Mechanical=misplacement/Rotation: [1=n 02=0 (3=0 URI=O UR2=O UR3=0 话Baun在 ry Con正重过热 BC-1 Iyp: Displacenent/Rots ion. 只4-1(+41Can) Ragien: Picked Edit Racier Dsrs:(Global)EdL.Cr eale. nitril Fimm l forn 凹: 回E 回m3 y crate maintained in subsequent steps. 28建立Mesh, Mesh Type: Element Type=C3D20R 且。身 生,品 2 2.9 Et L Job, Create Job: Name=Job-2 Model=Model-2: Submit t Data Cheak □suit COry 210查看计算结果Ⅴ Visualization: Plot Contours on Deformed Shape: u Magtinude 下国 Bb-2,出,Bba门d91ed T8:00生0 Em计的“ Scale(o+a+e2

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    Burgess_ni 就是个超简单的实例,算不上教程
    2020-09-24
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