声振论坛

 找回密码
 我要加入

QQ登录

只需一步,快速开始

查看: 2303|回复: 11

[转帖][分享]24种材料属性实例

[复制链接]
发表于 2006-4-1 01:53 | 显示全部楼层 |阅读模式

马上注册,结交更多好友,享用更多功能,让你轻松玩转社区。

您需要 登录 才可以下载或查看,没有账号?我要加入

x
Isotropic Elastic: High Carbon Steel <BR>MPMOD,1,1   <BR>MP,ex,1,210e9  ! Pa <BR>MP,nuxy,1,.29  ! No units <BR>MP,dens,1,7850  ! kg/m3 <BR><BR>Orthotropic Elastic: Al203 <BR>MPMOD,1,2   <BR>MP,ex,1,307e9  ! Pa <BR>MP,ey,1,358.1e9  ! Pa <BR>MP,ez,1,358.1e9  ! Pa <BR>MP,gxy,126.9e9  ! Pa <BR>MP,gxz,126.9e9  ! Pa <BR>MP,gyz,126.9e9  ! Pa <BR>MP,nuxy,1,.20  ! No units <BR>MP,nuxz,1,.20  ! No units <BR>MP,nuyz,1,.20  ! No units <BR>MP,dens,1,3750  ! kg/m3 <BR><BR>Anisotropic Elastic: Cadmium <BR>MPMOD,1,3   <BR>MP,dens,3400  ! kg/m3 <BR>TB,ANEL,1   <BR>TBDATA,1,121.0e9  ! C11 (Pa) <BR>TBDATA,2,48.1e9  ! C12 (Pa) <BR>TBDATA,3,121.0e9  ! C22 (Pa) <BR>TBDATA,4,44.2e9  ! C13 (Pa) <BR>TBDATA,5,44.2e9  ! C23 (Pa) <BR>TBDATA,6,51.3e9  ! C33 (Pa) <BR>TBDATA,10,18.5  ! C44 (Pa) <BR>TBDATA,15,18.5  ! C55 (Pa) <BR>TBDATA,21,24.2  ! C66 (Pa) <BR><BR>Blatz-K Rubber <BR>MPMOD,1,5   <BR>MP,gxy,1,104e7  ! Pa <BR><BR>Mooney-Rivlin: Rubber <BR>MPMOD,1,8   <BR>MP,dens,1,.0018  ! lb/in3 <BR>MP,nuxy,1,.499  ! No units <BR>TB,MOONEY,1   <BR>TBDATA,1,80  ! C10 (psi) <BR>TBDATA,2,20  ! C01 (psi) <BR><BR>Viscoelastic: G-11 Glass <BR>MPMOD,1,18   <BR>MP,dens,1,2390  ! kg/m3 <BR>TB,EVISC,1   <BR>TBDATA,46,27.4e9  ! Go (Pa) <BR>TBDATA,47,0.0  ! (Pa) <BR>TBDATA,48,60.5e9  ! Bulk modulus (Pa) <BR>TBDATA,61,.53  ! 1/ <BR><BR>Bilinear Isotropic Plasticity: Nickel Alloy <BR>MPMOD,1,6   <BR>MP,ex,1,180e9  ! Pa <BR>MP,nuxy,1,.31  ! No units <BR>MP,dens,1,8490  ! kg/m3 <BR>TB,BISO,1   <BR>TBDATA,1,900e6  ! Yield stress (Pa) <BR>TBDATA,2,445e6  ! Tangent modulus (Pa) <BR><BR>Transversely Anisotropic Elastic Plastic: 1010 Steel <BR>MPMOD,1,10   <BR>MP,ex,1,207e9  ! Pa <BR>MP,nuxy,1,.29  ! No units <BR>MP,dens,1,7845  ! kg/m3 <BR>TB,PLAW,,,,7   <BR>TBDATA,1,128.5e6  ! Yield stress (Pa) <BR>TBDATA,2,202e5  ! Initial strain at failure <BR>TBDATA,3,1.41  ! r-value <BR>TBDATA,4,1  ! Yield stress vs. plastic strain curve (see EDCURVE below) <BR>Strain(1) = 0,.05,.1,.15,.2 <BR>YldStres(1)=207e6,210e6,214e6,218e6,220e6 ! yield stress <BR>EDCURVE,ADD,1,Strain (1),YldStres(1) <BR><BR>Rate Sensitive Powerlaw Plasticity: A356 Aluminum <BR>MPMOD,1,17   <BR>MP,ex,1,75e9  ! Pa <BR>MP,nuxy,1,.33  ! No units <BR>MP,dens,1,2750  ! kg/m3 <BR>TB,PLAW,,,,4   <BR>TBDATA,1,1.002  ! k (MPa) <BR>TBDATA,2,.7  ! m <BR>TBDATA,3,.32  ! n <BR>TBDATA,4,5.0  ! Initial strain rate (s-1) <BR><BR>Plastic Kinematic: 1018 Steel <BR>MPMOD,1,19   <BR>MP,ex,1,200e9  ! Pa <BR>MP,nuxy,1,.27  ! No units <BR>MP,dens,1,7865  ! kg/m3 <BR>TB,PLAW,,,,1   <BR>TBDATA,1,310e6  ! Yield stress (Pa) <BR>TBDATA,2,763e6  ! Tangent modulus (Pa) <BR>TBDATA,4,40.0  ! C (s-1) <BR>TBDATA,5,5.0  ! P <BR>TBDATA,6,.75  ! Failure strain <BR><BR>Bilinear Kinematic Plasticity: Titanium Alloy <BR>MPMOD,1,33   <BR>MP,ex,1,100e9  ! Pa <BR>MP,nuxy,1,.36  ! No units <BR>MP,dens,1,4650  ! kg/m3 <BR>TB,BKIN,1   <BR>TBDATA,1,70e6  ! Yield stress (Pa) <BR>TBDATA,2,112e6  ! Tangent modulus (Pa) <BR><BR>Powerlaw Plasticity: Aluminum 1100 <BR>MPMOD,1,21   <BR>MP,ex,1,69e9  ! Pa <BR>MP,nuxy,1,.33  ! No units <BR>MP,dens,1,2710  ! kg/m3 <BR>TB,PLAW,,,,2   <BR>TBDATA,1,0.598  ! k <BR>TBDATA,2,0.216  ! n <BR>TBDATA,3,6500.0  ! C (s-1) <BR>TBDATA,4,4.0  ! P <BR><BR>3 Parameter Barlat Plasticity: Aluminum 5182 <BR>MPMOD,1,22   <BR>MP,ex,1,76e9  ! Pa <BR>MP,nuxy,1,.34  ! No units <BR>MP,dens,1,2720  ! kg/m3 <BR>TB,PLAW,,,,3   <BR>TBDATA,1,1  ! Hardening rule of 1 (yield stress) <BR>TBDATA,2,25e6  ! Tangent modulus (Pa) <BR>TBDATA,3,145e6  ! Yield stress (Pa) <BR>TBDATA,4,0.170  ! Barlat exponent, m <BR>TBDATA,5, .73  ! R00 <BR>TBDATA,6,.68  ! R45 <BR>TBDATA,7,.65  ! R90 <BR>TBDATA,8,0  ! CSID <BR><BR>Barlat Anisotropic Plasticity: 2008-T4 Aluminum <BR>MPMOD,1,23   <BR>MP,ex,1,76e9  ! Pa <BR>MP,nuxy,1,.34  ! No units <BR>MP,dens,1,2720  ! kg/m3 <BR>TB,PLAW,,,,6   <BR>TBDATA,1,1.04  ! k (MPa) <BR>TBDATA,2,.65  ! Initial strain at failure <BR>TBDATA,3,.254  ! n <BR>TBDATA,4,11  ! Barlat exponent, m <BR>TBDATA,5, 1.017  ! a <BR>TBDATA,6,1.023  ! b <BR>TBDATA,7,.9761  ! c <BR>TBDATA,8,.9861  ! f <BR>TBDATA,9,.9861  ! g <BR>TBDATA,9,.8875  ! h <BR><BR>Strain Rate Dependent Plasticity: 4140 Steel <BR>MPMOD,1,24   <BR>MP,ex,1,209e9  ! Pa <BR>MP,nuxy,1,.29  ! No units <BR>MP,dens,1,7850  ! kg/m3 <BR>TB,PLAW,,,,5   <BR>TBDATA,1,1  ! LCID yield stress vs. strain rate (see first EDCURVE command below) <BR>TBDATA,2,22e5  ! Tangent modulus (Pa) <BR>TBDATA,3,2  ! LCID Elastic modulus vs. strain rate (see second EDCURVE command below) <BR>StrnRate(1) = 0,.08,.16,.4,1.0 <BR>YldStres(1) = 207e6,250e6,275e6,290e6,300e6 <BR>ElasMod(1) = 209e9,211e9,212e9,215e9,218e9 <BR>EDCURVE,ADD,1,StrnRate(1),YldStres(1) <BR>EDCURVE,ADD,2,StrnRate(1),ElasMod(1) <BR><BR>Piecewise Linear Plasticity: High Carbon Steel <BR>MPMOD,1,28   <BR>MP,ex,1,207e9  ! Pa <BR>MP,nuxy,1,.30  ! No units <BR>MP,dens,1,7830  ! kg/m3 <BR>TB,PLAW,,,,8   <BR>TBDATA,1,207e6  ! Yield stress (Pa) <BR>TBDATA,3,.75  ! Failure strain <BR>TBDATA,4,40.0  ! C (strain rate parameter) <BR>TBDATA,5,5.0  ! P (strain rate parameter) <BR>TBDATA,6,1  ! LCID for true stress vs. true strain (see EDCURVE below) <BR>TruStran(1)=0,.08,.16,.4,.75 <BR>TruStres(1)=207e6,250e6,275e6,290e6,3000e6 <BR>EDCURVE,ADD,1,TruStran (1),TruStres(1) <BR><BR>Johnson-Cook Linear Polynomial EOS: 1006 Steel <BR>MPMOD,1,30   <BR>MP,ex,1,207e9  ! Pa <BR>MP,nuxy,1,.30  ! No units <BR>MP,dens,1,7850  ! kg/m3 <BR>TB,EOS,1,,,1,1   <BR>TBDATA,1,350.25e6  ! A (Pa) <BR>TBDATA,2,275e6  ! B (Pa) <BR>TBDATA,3,.36  ! n <BR>TBDATA,4,.022  ! c <BR>TBDATA,5,1.0  ! m <BR>TBDATA,6,1400  ! Melt temperature (oC) <BR>TBDATA,7,30  ! Room temperature (oC) <BR>TBDATA,8,10  ! Initial strain rate <BR>TBDATA,9,4500  ! Specific heat <BR>TBDATA,10,240e6  ! Failure stress <BR>TBDATA,11,-.8  ! Failure value D1 <BR>TBDATA,12,2.1  ! Failure value D2 <BR>TBDATA,13,-.5  ! Failure value D3 <BR>TBDATA,14,.0002  ! Failure value D4 <BR>TBDATA,15,.61  ! Failure value D5 <BR>TBDATA,17,20e5  ! EOS linear polynomial term <BR><BR>Johnson-Cook Gruneisen EOS: OFHC Copper <BR>MPMOD,1,31   <BR>MP,ex,1,138e9  ! Pa <BR>MP,nuxy,1,.35  ! No units <BR>MP,dens,1,8330  ! kg/m3 <BR>TB,EOS,1,,,1,2   <BR>TBDATA,1,89.63e6  ! A (Pa) <BR>TBDATA,2,291.64e6  ! B (Pa) <BR>TBDATA,3,.31  ! n <BR>TBDATA,4,.025  ! c <BR>TBDATA,5,1.09  ! m <BR>TBDATA,6,1200  ! Melt temperature (oC) <BR>TBDATA,7,30  ! Room temperature (oC) <BR>TBDATA,8,10  ! Initial strain rate <BR>TBDATA,9,4400  ! Specific heat <BR>TBDATA,10,240e6  ! Failure stress <BR>TBDATA,11,-.54  ! Failure value D1 <BR>TBDATA,12,4.89  ! Failure value D2 <BR>TBDATA,13,-3.03  ! Failure value D3 <BR>TBDATA,14,.014  ! Failure value D4 <BR>TBDATA,15,1.12  ! Failure value D5 <BR>TBDATA,16,.394  ! C <BR>TBDATA,17,1.489  ! S1 <BR>TBDATA,18,0.0  ! S2 <BR>TBDATA,19,0.0  ! S3 <BR>TBDATA,20,2.02  ! 0 <BR>TBDATA,21,.47  ! A <BR><BR>Null Material Linear Polynomial EOS: Brass <BR>MPMOD,1,32   <BR>MP,ex,1,200e9  ! Pa <BR>MP,nuxy,1,.3  ! No units <BR>MP,dens,1,7500  ! kg/m3 <BR>TB,EOS,1,,,2,1   <BR>TBDATA,1,0.0  ! Pressure cut-off <BR>TBDATA,3,1.5  ! Relative volume in tension <BR>TBDATA,4,.7  ! Relative volume in compression <BR>TBDATA,17,16e5  ! EOS linear polynomial <BR><BR>Null Material Gruneisen EOS: Aluminum <BR>MPMOD,1,29   <BR>MP,ex,1,100e9  ! Pa <BR>MP,nuxy,1,.34  ! No units <BR>MP,dens,1,2500  ! kg/m3 <BR>TB,EOS,1,,,2,2   <BR>TBDATA,1,-10000  ! Pressure cut-off (Pa) <BR>TBDATA,3,2.0  ! Relative volume in tension <BR>TBDATA,4,.5  ! Relative volume in compression <BR>TBDATA,16,.5386  ! C <BR>TBDATA,17,1.339  ! S1 <BR>TBDATA,18,0.0  ! S2 <BR>TBDATA,19,0.0  ! S3 <BR>TBDATA,20,1.97  ! 0 <BR>TBDATA,21,.48  ! A <BR><BR>Rigid Material: Steel <BR>MPMOD,1,7   <BR>MP,ex,1,207e9  ! Pa <BR>MP,nuxy,1,.3  ! No units <BR>MP,dens,1,7580  ! kg/m3 <BR>EDMP,rigid,1,7,7   <BR><BR>Cable Material: Steel <BR>MPMOD,1,27   <BR>MP,ex,1,207e9  ! Pa <BR>MP,nuxy,1,.3  ! No units <BR>EDMP,cable,1,1  ! See EDCURVE below <BR>EngStran(1) = .02,.04,.06,.08 <BR>EngStres(1) = 207e6,210e6,215e6,220e6 <BR>EDCURVE,ADD,1,EngStran (1),EngStres(1) <BR><BR>Transversely Anisotropic FLD: Stainless Steel <BR>MPMOD,1,54   <BR>MP,ex,1,30e6  ! Pa <BR>MP,nuxy,1,.29  ! No units <BR>MP,dens,1,.00285  ! kg/m3 <BR>TB,PLAW,1,,,10   <BR>TBDATA,1,20e3  ! Initial yield stress (Pa) <BR>TBDATA,2,5000  ! Tangent modulus (Pa) <BR>TBDATA,3,.2  ! Hardening parameter <BR>TBDATA,5,1  ! Maximum yield stress curve (see EDCURVE below) <BR>mnstrn(1) = -30,-10,0,20,40,50 <BR>mjstrn(1) = 80,40,29,39,45,44 <BR>EDCURVE,ADD,1,mnstrn (1),mjstrn(1) <BR><BR>Steinberg Gruneisen EOS: Stainless Steel <BR>MPMOD,1,52   <BR>MP,gxy,1,11.16e6  ! (Pa) <BR>MP,dens,1,.285  ! (kg/m3) <BR>TB,EOS,1,,,5,2   <BR>TBDATA,1,49.3e3  ! Initial yield stress (Pa) <BR>TBDATA,2,43  ! Hardening coefficient <BR>TBDATA,3,.35  ! n <BR>TBDATA,5,.36e6  ! Maximum yield stress (Pa) <BR>TBDATA,10,32  ! Atomic weight <BR>TBDATA,11,2380  ! Absolute melting temp. <BR>TBDATA,15,2  ! Spall type <BR>TBDATA,16,1  ! Cold compression energy flag <BR>TBDATA,17,-50  ! Min. temp. parameter <BR>TBDATA,18,200  ! Max. temp. parameter <BR>TBDATA,29,.457  ! C <BR>TBDATA,30,1.49  ! S1 <BR>TBDATA,31,0.0  ! S2 <BR>TBDATA,32,0.0  ! S3 <BR>TBDATA,33,1.93  ! 0 <BR>TBDATA,34,1.4  ! A <BR>
回复
分享到:

使用道具 举报

发表于 2006-4-1 10:21 | 显示全部楼层
有中文的吗<BR><BR>好象不太明白<BR><BR>看不懂啊
发表于 2006-4-1 18:44 | 显示全部楼层
从帮助里直接复制过来的吧,楼主。
发表于 2006-4-1 19:02 | 显示全部楼层
谢谢
 楼主| 发表于 2006-4-2 00:55 | 显示全部楼层

回复:(AaronSpark)[转帖][分享]24种材料属性实例

别的论坛看到的就顺手贴过来了
发表于 2006-7-18 20:08 | 显示全部楼层
谢了
发表于 2006-7-18 22:58 | 显示全部楼层
看起来挺好的,不过没有具体说明那种材料啊
发表于 2006-7-18 23:05 | 显示全部楼层
仔细看了看,基本能看懂,不过我见过课本后面有这个,那是中文的,现在该成命令六了
发表于 2006-7-19 09:20 | 显示全部楼层
好东西,用中文解释一下会更好!!
发表于 2006-7-19 10:44 | 显示全部楼层
什么书上有这个中文的解释啊?能不能麻烦你把中文的给粘上啊?
发表于 2006-7-19 10:46 | 显示全部楼层
各种材料的适用性如果不是很了解的话,直接粘贴肯定会出问题的
发表于 2006-7-19 17:49 | 显示全部楼层
这些材料特性在网上很好找的!
您需要登录后才可以回帖 登录 | 我要加入

本版积分规则

QQ|小黑屋|Archiver|手机版|联系我们|声振论坛

GMT+8, 2024-12-3 10:55 , Processed in 0.070118 second(s), 19 queries , Gzip On.

Powered by Discuz! X3.4

Copyright © 2001-2021, Tencent Cloud.

快速回复 返回顶部 返回列表