加载中…加载中…加载中…
总想用特别的方式去追寻这段特别的往日
却怎么也发现不了自己在何方
远方亲爱的你,是否在天上观望着我,想念着我
曾经多少个温柔的夜晚
曾经多少个动人的微笑
曾经多少个热烈的拥抱
曾经多少个无知的傻笑
总以为不远的将来还能相见
总希望你过得比我要好
我知道这段凄凉的音乐
刺痛着我的心
却怎么也找不到你那美丽的脸庞
听着你朋友的述说
我将永远负你这段拥抱
从开始到结尾也许能隐约感受到你的心跟我一起在跳
却不想得来的竞是如此的结局
我恨自己当初为什么没有去坚持
为什么不能给你坚定的依靠
明知道你的心很糟,却老想着时间会慢慢淡化掉
一年多了,我总以为你只是残,或废了,可恶大卡车却将你永远带走了
怎么也想不到你就这么走了
你一直都让着我,你也知道得到的不一定拥有
所以你坚持我走我的路
可你的心在痛,眼在红
小芳,我的初爱和恋人,我只有深深把你埋在心里
我会找个时间去看你,希望你在另一个世界快快乐乐,高高兴兴.
（１）框架结构分析
/prep7
mp,ex,1,206000
mp,prxy,1,0.304
tb,bkin,1
tbdata,1,275,2060
r,1,,
et,1,beam188,
keyopt,1,6,3
keyopt,1,7,1
sectype,1,beam,i,beam,
secdata,300,300,150,9,9,6.5
sectype,2,beam,i,column,
secdata,200,200,200,12,12,8
k,1,0,0,0
k,2,0,2600,0
k,3,3600,0,0
k,4,3600,2600,0
k,100,-2000,2600,0
k,200,1800,4800,0
l,1,2
l,3,4
l,2,4
lsel,s,,,1,2
latt,1,1,1,,100,,2
lesize,all,,,26,
lsel,s,,,3
latt,1,1,1,,200,,1
lesize,all,,,36,
lsel,all
lmesh,all
allsel,all
版本不近相同
（１）
fini
/clear
/prep7
rid=1.35
rsd=0.12
et,1,56,,,1
et,2,169
et,3,171
tb,hyper,1,1,2,mooney
tbdata,1,80.0,20,0.002
mp,nuxy,1,.49
mp,mu,2,0.0
r,2,,,1,0.1
r,3,,,1,0.1
!*
local,11,1,rid+rsd/2
wpcsys,11
pcirc,rsd/2,,0,90
pcirc,rsd/2,,90,180
pcirc,rsd/2,,180,270
pcirc,rsd/2,,270,360
nummrg,kp
eshape,2
esize,.015
amesh,all
!
csys,0
k,20,rid-rsd,-rsd/2
k,21,rid+(2*rsd),-rsd/2
k,22,rid+(2*rsd),rsd/2
k,23,rid+(2*rsd),rsd/2
k,24,rid-rsd,rsd/2
l,21,20
l,22,21
l,24,23
!*
type,2
mat,2
real,2
lmesh,6
lmesh,9
real,3
lmesh,11
kmesh,24
csys,11
nsel,s,loc,x,rsd/2
type,3
real,2
esurf
real,3
esurf
esel,all
nsel,all
d,all,uz,0
n_load=node(kx(24),ky(24),0)
nplot
/user
save,oring,db
1. If you are modeling incompressible
flow, the pressure drop will be the quantity of interest and not
the actual pressure value.
2. Fluent will fix the pressure at a particular location based on
either the value at a pressure boundary or the location specified
in Operating condition panel. Hence, it is possible to get negative
pressure value for an incompressible flow problem.
3. Please check the results of steady state solution for pressure
distribution. If the pressure distribution is quite different from
the value you obtained after time step-1, please recheck the
changes you have made while shifting from steady state to transient
state simulation.
| 分类： Fluent技术 |
解决办法：右键单击快捷方式，把目标由x:\fluent.inc\ntbin\ntx86\fluent.exe
改成： x:\fluent.inc\ntbin\ntx86\fluent.exe 2d -driver msw
如果还有三维的，可以再建立一个快捷方式改成：
x:\fluent.inc\ntbin\ntx86\fluent.exe 3d -driver msw
这就可以直接调用了。
也有可能是和别的软件冲突，如MATLAB等使fluent无法显示图像。
rpsetvar flow-time 0.0
#include 'udf.h'
#include 'mem.h'
#include 'dynamesh_tools.h'
static real v_x = 0.0,v_y=0.0,omega_z=0.0;
DEFINE_CG_MOTION(piston,dt,vel,omega,time,dtime)
{
face_t f;
cell_t c;
real
f_glob[ND_ND],m_glob[ND_ND],x_cg[ND_ND],dv_x,dv_y,domega_z;
Domain *domain= Get_Domain (1);
Thread *tf1 = Lookup_Thread (domain, 3);
int i;
/* reset velocities */
NV_S(vel, =, 0.0);
NV_S(omega, =, 0.0);
if (!Data_Valid_P())
return;
for(i=0;i<=ND_ND;i++)
{
f_glob[i]=0;
m_glob[i]=0;
}
/* get the thread pointer for which this motion is defined */
for(i=0;i<ND_ND;i++)
x_cg[i]=DT_CG(dt)[i];
if(time<=0.001)
{
vel[1]=34.5;
Message ('\ntime=%f ,x=%.10lf ,y=%.10lf , force_x=%.1f
,force_y=%.1f ,moment_x=%f,moment_y=%f,moment_z=%f ,Vx=%f ,Vy=%f
,omega_z=%f\n',
time,x_cg[0],x_cg[1],f_glob[0],f_glob[1],m_glob[0],m_glob[1],m_glob[2],v_x,v_y,omega_
发博文