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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 。-Anderson the computational fluid mechanics and its application "chapter 7 quasi one-dimensional nozzle flow numerical solution of section 7.3 subsonic- supersonic isentropic nozzle flow of
xfoil6.96
- XFOIL is an interactive program for the design and analysis of subsonic isolated airfoils.
subsonic-3.4.beta1-src
- 在LINUX下基于GSTREAMER编写的多媒体播放器程序-LINUX-based GSTREAMER in the preparation of the multimedia player program
SubSonic
- SubSonic是一个ORM框架，或者说是一个代码生成器，它的工作流程和一般的ORM工具不同，所有的工作全是自动完成，生成完整的数据访问层类库，然后在工程中引用即可使用。整个过程很简单，-Use the framework
subsonic-SubSonic-3.0-3.0.0.4-15-g5b14d2b
- Subsonic，方便易用的ORM，支持数据库自动迁移和更新-Subsonic, easy to use ORM
AppBox55043
- AppBox v0.1.0 AppBox是企业综合管理系统的基础框架，包括菜单管理、人员管理、权限管理、组织结构管理等模块。 AppBox基于一些开源程序，比如ExtAspNet, SubSonic, log4net。 -AppBox v0.1.0 AppBox is based enterprise framework for integrated management system, including menu management, personnel managem
fortran-files
- 文件1.f90：生成翼型naca0012的椭圆网格，并计算流场，给出壁面压力分布 文件2.f90：maccormack方法解一维burger s方程 文件3.f90：解一维laval管流动，其进出口均为亚音速，喉道后部有激波-File 1.f90: generate the airfoil naca0012 elliptical rotary cell, and calculate the flow field, given the wall pressure distributio
charpt7_5
- 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。自己编写matlab源代码。-Anderson the computational fluid mechanics and its application "chapter 7 quasi one-dimensional nozzle flow numerical solution of section 7.5 then theory subsonic- supersoni
Vortex-lattice-FORTRAN-planforms
- fortran语言的涡格法估算亚音速流场特性的程序文档和方法-vortex lattice method estimates fortran language subsonic flow field characteristics of program documentation and methods
panair
- 亚声速超声速高阶空气动力学板块代码。所有线化理论板块方法中最可信和准确的。-High order aerodynamic panel code. The most versatile and accurate of all the linear theory panel codes. Subsonic/supersonic solutions with linear source strength variation and quadratic doublet strength variatio
yashengsuchashengsuliudong
- 利用MacCormark算法，解二维拉瓦尔喷管亚声速到超声速流问题-To use MacCormark algorithm, solution Villa Val nozzle subsonic to supersonic flow problem
NND-subsonic
- fortran编写的一维标量问题的求解代码，格式为NND，亚声速来流。-to solve the problem of one-dimensional scalar code written in fortran format NND, subsonic flow.
one-dimensional-internal-flow-CFD
- 一维管流MC格式，含出口超音速和亚音速两个算例-One-dimensional pipe flow MC format, including export supersonic and subsonic two examples
20090205maolz
- 因为我的网站空间到期了，原先是asp的,现在升级成asp.net,所以花了个星期做了这个版本，应该算是这个网站的第三版了，第一版是我初学网站制作时做的，第二版是学asp时做的http://mlzboy.jahee.com，用的是nowa整站的修改版，第三版就是现在这一版是我自己做的。 我制作这个版本的终止是够用就行，满足自己的要求就行。由于本人是做后台的，因此前台的div+css+javascr ipt部分并没有什么建树，如果你对生成的代码要求非常高，可能这个程序就不适用于你了。如果你是后台
Lawaer2
- 准一维，拉瓦尔喷管全亚声速非守恒型方程求解-Quasi one dimensional, Lawal nozzle subsonic non conservation equation
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
CFD7_5
- 亚音速-超音速等熵喷管，守恒形式方程,MacCormack方法求解-Subsonic- supersonic isentropic nozzle, conservation equation form, MacCormack method for solving
TTM2
- 这是一个鼓包通道的网格生成程序，用于计算亚声速、跨声速、超声速的无粘流动。-This is an grid generate code for channel with a circular arc bump it is used for compute subsonic/supersonic flow.
CFD
- 计算进口边界条件为超音和亚音条件下，气流流经凸包时的二维流动状况-program for calculate air flows through the convex hullto in the import boundary conditions of supernic and subsonic
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