PATRAN,PATRAN,在线英语词典,英文翻译,专业英语

1) PATRAN

PATRAN

Development of Rapid Dynamics Modeling System of Machine Tool Based on PATRAN;

基于PATRAN的机床结构快速动力学建模系统的开发

The Secondary Development of Structural Optimization Program System Based on MSC.Patran/Nastran;

基于MSC.Patran/Nastran的结构优化程序系统的二次开发

Interface realization between Fluent and Patran and its application in ship mechanics;

Fluent与Patran的接口实现及其在船舶力学中的应用

2) MSC Patran

MSC Patran

Analysis of Interlayer Structure of Composite Material by MSC Patran/Nastran;

利用MSC Patran/Nastran分析复合材料夹层结构

Application of MSC Patran in Modal Analysis of Buoyant Raft Shock-resistant System;

MSC Patran在浮筏隔振装置模态分析中的应用

System for Response Analysis to Impact of Floating Raft Based on MSC Patran;

基于MSC Patran的浮筏冲击动响应分析计算系统

3) Patran/Marc

Patran/Marc

By the application of Patran/Marc software,spur gear of diesel engine in the highest point of the single-tooth meshing is analyzed,the process of FEM is expatiated and distribution of the static stress is accessed.

以柴油发动机传动机构中的直齿轮作为研究对象,应用Patran/Marc软件,在主动齿轮单齿啮合的最高点,对该齿轮进行了应力分析,阐述了齿轮有限元分析的方法,对计算结果进行分析,获得齿轮等效应力分布图。

4) Patran/Nastran

Patran/Nastran

Modeling Using UG for Some Turbine Blade and Stress Analysis of Patran/Nastran FEM;

涡轮叶片的UG建模和Patran/Nastran有限元应力分析

Structural Optimization System Based on MSC.PATRAN/NASTRAN;

基于MSC.PATRAN/NASTRAN的结构优化程序系统

Finite Element Analysis of Hatch in PATRAN/NASTRAN;

舱盖结构的PATRAN/NASTRAN有限元分析

5) MSC/PATRAN

MSC/PATRAN

Development of Test Data Tracking, Analyzing and Processing System for Aircraft Structural Strength Based on MSC/PATRAN Platform;

基于MSC/PATRAN的飞机结构强度静力试验数据实时跟踪与处理系统开发

Use C++ builder language to control MSC/PATRAN;

用C++Builder语言实现对MSC/PATRAN的控制

In this paper,firstly we built a finite element model of the folding wing by MSC/PATRAN and solved the main vibration modes in case of varied folding angles by NASTRAN.

在本文中,首先用MSC/PATRAN建立了折叠翼的有限元模型,然后用NASTRAN求解出折叠翼在各折叠角下的主要振动模态。

6) MSC/PATRAN

流体边界元

For comparison,the finite element model is built with MSC/PATRAN and the method combining fluid Boundary Element Method and the experimental formula is also carried out with MSC/NASTRAN.

用MSC/PATRAN建立有限元模型 ,在MSC/NASTRAN平台上主要对流体边界元法、经验公式法进行结构的流体附加质量计算的对比研究和计算。

参考词条

MSC.Nastran/Patran Patran/Dytran Patran modeling Msc patran software MSC·Patran/Nastran MSC Patran & Nastran Patran Command Language 现代交通运输 S-蛋白

补充资料：ANSYS模型转到MSC.MARC

！ANSYS命令流
! 写单元及节点数据文件
! 作者：陆新征，清华大学土木系
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
!选中所有单元
ALLSEL,ALL
! 得到当前模型中的总节点数
*GET,NNode,NODE,,COUNT, , , ,
!输出节点
*CFOPEN,Node,txt
*VWRITE
('coordinates')
*VWRITE,chrval(3),chrval(NNode),chrval(0),chrval(1)
(4A5)
*DO,I,1,NNode
*VWRITE,I,NX(I),NY(I),NZ(I)
(F8.0,3F13.5)
*ENDDO
*CFCLOS

!打开单元文件
*CFOPEN,ELEM,txt
!得到所有单元数
ESEL,S,ENAME,,65
ALLSEL,ALL
*GET,NElem,ELEM,,COUNT, , , ,
*VWRITE,chrval(NElem)
('Number of Element: ', A8)
!对单元集进行循环
*DO,I,1,NElem
!得到当前单元的类型
*GET,ENAME,ELEM,I,ATTR,ENAM
!如果是65号(65号单元)
*IF,ENAME,EQ,65,THEN
!得到该单元的节点编号
*GET,EN1,ELEM,I,NODE,1
*GET,EN2,ELEM,I,NODE,2
*GET,EN3,ELEM,I,NODE,3
*GET,EN4,ELEM,I,NODE,4
*GET,EN5,ELEM,I,NODE,5
*GET,EN6,ELEM,I,NODE,6
*GET,EN7,ELEM,I,NODE,7
*GET,EN8,ELEM,I,NODE,8
*VWRITE,I,EN1,EN2,EN3,EN4,EN5,EN6,EN7,EN8
(F8.0,8F8.0)
*END IF
*ENDDO
*CFCLOS

!Fortran程序，把ansys结果转换为MARC模型文件格式
program main
implicit none;
integer Key;
write(*,*) "Input 1 for node, 2 for element"
read(*,*) Key
if (Key==1) then
call Node_IO()
end if
if (Key==2) then
call Elem_IO()
end if
stop
end program

subroutine Node_IO()
implicit none
integer NNode,I, J
real*8,pointer :: Node(:,:)
real*8 x;
character :: filename*10;
write(*,*) "Please input node filename"
read(*,'(A10)') filename
open(66,file=filename)
read(66,*) NNode
allocate (Node(NNode,3))
do I=1,NNode
read(66,*) x, (Node(I,J), J=1,3)
end do
close (66)
filename=filename//"NEW"
open (66,file=filename)
write(66,'(4I10)') 3, NNode, 0, 1
do I=1, NNode
write(66,'(I10, 3E20.8)') I, (Node(I,J), J=1,3)
end do
close (66)
return
end subroutine Node_IO

subroutine Elem_IO()
implicit none
integer NElem,NumNode,ElemTyp,I, J
integer,pointer :: Elem(:,:)
real*8 x;
real*8,pointer :: y(:)
character :: filename*10, outformat*11,CharEtype;
write(*,*) "Please input node filename"
read(*,'(A10)') filename
write(*,*) "Please input Element type & Number of Nodes per element"

说明：补充资料仅用于学习参考，请勿用于其它任何用途。

首页 \| 翻译 \| 影视 \| 论坛 \| 索引 Patran software MSC Patran

1) PATRAN PATRAN 1. Development of Rapid Dynamics Modeling System of Machine Tool Based on PATRAN; 基于PATRAN的机床结构快速动力学建模系统的开发 2. The Secondary Development of Structural Optimization Program System Based on MSC.Patran/Nastran; 基于MSC.Patran/Nastran的结构优化程序系统的二次开发 3. Interface realization between Fluent and Patran and its application in ship mechanics; Fluent与Patran的接口实现及其在船舶力学中的应用 2) MSC Patran MSC Patran 1. Analysis of Interlayer Structure of Composite Material by MSC Patran/Nastran; 利用MSC Patran/Nastran分析复合材料夹层结构 2. Application of MSC Patran in Modal Analysis of Buoyant Raft Shock-resistant System; MSC Patran在浮筏隔振装置模态分析中的应用 3. System for Response Analysis to Impact of Floating Raft Based on MSC Patran; 基于MSC Patran的浮筏冲击动响应分析计算系统 3) Patran/Marc Patran/Marc 1. By the application of Patran/Marc software,spur gear of diesel engine in the highest point of the single-tooth meshing is analyzed,the process of FEM is expatiated and distribution of the static stress is accessed. 以柴油发动机传动机构中的直齿轮作为研究对象,应用Patran/Marc软件,在主动齿轮单齿啮合的最高点,对该齿轮进行了应力分析,阐述了齿轮有限元分析的方法,对计算结果进行分析,获得齿轮等效应力分布图。 4) Patran/Nastran Patran/Nastran 1. Modeling Using UG for Some Turbine Blade and Stress Analysis of Patran/Nastran FEM; 涡轮叶片的UG建模和Patran/Nastran有限元应力分析 2. Structural Optimization System Based on MSC.PATRAN/NASTRAN; 基于MSC.PATRAN/NASTRAN的结构优化程序系统 3. Finite Element Analysis of Hatch in PATRAN/NASTRAN; 舱盖结构的PATRAN/NASTRAN有限元分析 5) MSC/PATRAN MSC/PATRAN 1. Development of Test Data Tracking, Analyzing and Processing System for Aircraft Structural Strength Based on MSC/PATRAN Platform; 基于MSC/PATRAN的飞机结构强度静力试验数据实时跟踪与处理系统开发 2. Use C++ builder language to control MSC/PATRAN; 用C++Builder语言实现对MSC/PATRAN的控制 3. In this paper,firstly we built a finite element model of the folding wing by MSC/PATRAN and solved the main vibration modes in case of varied folding angles by NASTRAN. 在本文中,首先用MSC/PATRAN建立了折叠翼的有限元模型,然后用NASTRAN求解出折叠翼在各折叠角下的主要振动模态。 6) MSC/PATRAN 流体边界元 1. For comparison,the finite element model is built with MSC/PATRAN and the method combining fluid Boundary Element Method and the experimental formula is also carried out with MSC/NASTRAN. 用MSC/PATRAN建立有限元模型 ,在MSC/NASTRAN平台上主要对流体边界元法、经验公式法进行结构的流体附加质量计算的对比研究和计算。参考词条 MSC.Nastran/Patran Patran/Dytran Patran modeling Msc patran software MSC·Patran/Nastran MSC Patran & Nastran Patran Command Language 现代交通运输 S-蛋白补充资料：ANSYS模型转到MSC.MARC ！ANSYS命令流 ! 写单元及节点数据文件 ! 作者：陆新征，清华大学土木系 !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! !选中所有单元 ALLSEL,ALL ! 得到当前模型中的总节点数 GET,NNode,NODE,,COUNT, , , , !输出节点 CFOPEN,Node,txt VWRITE ('coordinates') VWRITE,chrval(3),chrval(NNode),chrval(0),chrval(1) (4A5) DO,I,1,NNode VWRITE,I,NX(I),NY(I),NZ(I) (F8.0,3F13.5) ENDDO CFCLOS !打开单元文件 CFOPEN,ELEM,txt !得到所有单元数 ESEL,S,ENAME,,65 ALLSEL,ALL GET,NElem,ELEM,,COUNT, , , , VWRITE,chrval(NElem) ('Number of Element: ', A8) !对单元集进行循环 DO,I,1,NElem !得到当前单元的类型 GET,ENAME,ELEM,I,ATTR,ENAM !如果是65号(65号单元) IF,ENAME,EQ,65,THEN !得到该单元的节点编号 GET,EN1,ELEM,I,NODE,1 GET,EN2,ELEM,I,NODE,2 GET,EN3,ELEM,I,NODE,3 GET,EN4,ELEM,I,NODE,4 GET,EN5,ELEM,I,NODE,5 GET,EN6,ELEM,I,NODE,6 GET,EN7,ELEM,I,NODE,7 GET,EN8,ELEM,I,NODE,8 VWRITE,I,EN1,EN2,EN3,EN4,EN5,EN6,EN7,EN8 (F8.0,8F8.0) END IF ENDDO CFCLOS !Fortran程序，把ansys结果转换为MARC模型文件格式 program main implicit none; integer Key; write(,) "Input 1 for node, 2 for element" read(,) Key if (Key==1) then call Node_IO() end if if (Key==2) then call Elem_IO() end if stop end program subroutine Node_IO() implicit none integer NNode,I, J real8,pointer :: Node(:,:) real8 x; character :: filename10; write(,) "Please input node filename" read(,'(A10)') filename open(66,file=filename) read(66,) NNode allocate (Node(NNode,3)) do I=1,NNode read(66,) x, (Node(I,J), J=1,3) end do close (66) filename=filename//"NEW" open (66,file=filename) write(66,'(4I10)') 3, NNode, 0, 1 do I=1, NNode write(66,'(I10, 3E20.8)') I, (Node(I,J), J=1,3) end do close (66) return end subroutine Node_IO subroutine Elem_IO() implicit none integer NElem,NumNode,ElemTyp,I, J integer,pointer :: Elem(:,:) real8 x; real8,pointer :: y(:) character :: filename10, outformat11,CharEtype; write(,) "Please input node filename" read(,'(A10)') filename write(,) "Please input Element type & Number of Nodes per element" 说明：*补充资料仅用于学习参考，请勿用于其它任何用途。
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