搜索资源列表
THOMAS
- 安德森/计算流体力学/fortran源代码(第九章THOMAS算法)-Anderson/Computational Fluid Dynamics/fortran source code (Chapter THOMAS algorithm)
Source1
- 安德森计算流体力学入门7.3源程序,亚超音速喷嘴-Anderson Computational Fluid Dynamics Getting Started 7.3 source code
for-anderson-CFD-code
- 计算流体力学安德森第七章练习作业,附源程序-CFD Anderson Chapter VII practice operations, with source code. .
Charpt7_3
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解 7.3节 亚声速—超声速等熵喷管流动的CFD解法 。
shouhengxing
- 安德森《计算流体力学及其应用》第七章第五节再论亚声速-超声速等熵喷管流动的CFD解法-Anderson " computational fluid dynamics and its applications," Chapter VII Section V More on subsonic- CFD solution isentropic supersonic nozzle flow
laval_sub
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解,7.3Fortran程序-Numerical Solution of Anderson Computational Fluid Dynamics and Its Applications, Chapter VII of the proposed one-dimensional nozzle flow, Fortran program
laval_sup
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解,7.4Fortran程序-Numerical Solution of Anderson Computational Fluid Dynamics and Its Applications, Chapter VII of the proposed one-dimensional nozzle flow, 7.4Fortran program
laval_con
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解 7.5节 再论亚声速—超声速等熵喷管流动的CFD解法,Fortran程序-Anderson Computational Fluid Dynamics and Its Applications, Chapter VII of the quasi one-dimensional nozzle flow again on the numerical solution of 7.5 subsonic- supersonic isentrop
laval_shock
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解 7.6节激波捕捉Fortran程序-Anderson Computational Fluid Dynamics and Its Applications, Chapter VII of the quasi one-dimensional nozzle flow numerical solution 7.6 Fortran shock capturing process
7.37.4-0
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解, 7.3节7,4节matlab程序-Anderson Computational Fluid Dynamics and Its Applications Numerical Solution of one-dimensional nozzle flow Chapter VII of the proposed, section 7.3 7,4 matlab program
chapter10
- 《计算流体力学及其应用》第十章流过平板的超声速流动的数值解。安德森的书。fortran编写。-Based on John D. Anderson, JR., Chapter 10, In Computational Fluid Dynamics,
Task4
- 安德森的空气动力学大作业。计算激波前后的马赫数的特征线的。-Anderson s book. Aerodynamic.Ma number charactertistic line.
Task3B
- 安德森的空气动力学大作业。计算扩压器中背压改变引起的流动中马赫数的变化。和激波位置的移动。matlab编。-Anderson s book. Aerodynamic.When back pressure changes, Mach number changes.
task3A
- 安德森的空气动力学中在计算激波和马赫数的特征线时会用到一些公式和函数。-Anderson s book. Aerodynamic.some important function when calculating Ma number charactertistic line.
solution-
- 安德森《计算流体力学及其应用》第七章拟一维喷管流动的数值解 7.3节 亚声速—超声速等熵喷管流动的CFD解法 -CFD solution supersonic isentropic nozzle flow- Anderson " Computational Fluid Dynamics and Its Applications," Chapter VII of the quasi one-dimensional nozzle flow numerical solution of
esp8266important
- 安德森的的撒的地方大方法嘎嘎嘎复合肥大广高速(aad addda adaarfra aeraf aaaaaaaaaaart)
7
- 安德森计算流体力学基础第七章MATLAB实现(The seventh chapter MATLAB realization of Anderson computational fluid mechanics)
PetShop
- 北大青鸟S2 JAVAOOP 宠物商店 打算dad的撒打算安德森(Hello, everyone!I came from Laifeng in Hubei Enshi, which is a small developing town. My hobbies are walking, seeing scenery and cheating and.)
计算流体力学基础及其应用美.约翰D.安德森
- 计算流体力学书籍,详细介绍了有限差分方法以及编程的相关理论(Computational fluid mechanics books, in detail the finite difference method and programming theory.)
安德森《计算流体力学》源代码
- 计算流体力学源代码。。。。。。。。。。。。。。。(the Fortran code for CFD)