搜索资源列表
Flat_Plate
- 平板超声速流流场计算程序,安德森《计算流体力学及其应用》的第十章-Flat Plate Flow supersonic N-S
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
pmew
- 2维超音速流的Prandtl-Meyer膨胀破的fortran程序-2-dimensional supersonic flow of the Prandtl-Meyer expansion of breaking the fortran program
KE_Upgrading
- supersonic speed equation of motion
EFFECTS
- 本文应用重叠网格技术对子母弹分离过程中多体无粘超声速流动进行了数值仿真。采用 NND 格式,通过求解Euler 方程,给出了母弹附近的子弹气动干扰特性。-In this paper, separation of overlapping grid of cluster bombs during the multi-body inviscid supersonic flow of the numerical simulation. With NND format, by solving the
ycpenguan
- 拟一维亚声速---超音速等熵喷管流动的CFD解法-Via the speed of sound to be a supersonic isentropic nozzle flow--- the CFD solution
lyg
- 一维喷管流动数值模拟的全超声速解法,与其他的有一些区别-One-dimensional numerical simulation of the entire nozzle flow supersonic solution, there are some differences with other
TNTk_omeg
- TNTk_omega湍流模型的隐式解法及其在超声速流动模拟中的应用-TNTk_omega turbulence model in the implicit solution of supersonic flow simulation of
MAIN
- 本程序是采用先进的NND格式计算超音速突扩的流场。计算结果可以看出NND格式捕z捉激波能力还很强。-This procedure is the use of advanced computing NND scheme sudden expansion of the supersonic flow field. NND scheme results can be seen catching z catching ability is also a strong shock wave.
symmetry-TVD-shock
- 对称TVD查分算法求解超音速流在前台阶管道中的流动问题-Symmetric TVD to check sub-algorithm for solving flow problems in the supersonic flow in the former step pipeline
supersonic-flow-over-flat-plate
- 利用显示MacCormack时间步计算二维超声速绕平板流,对于研究计算流体力学有很大帮助-A Fortran program of two-dimensional Navier-Stokes equations for the supersonic flow over a flat plate based on MacCormack s explicit time-marching technique.
charpt10_4
- 安德森《计算流体力学及其应用》第十章流过平板的超声速流动 10.4节 纳维—斯托克斯方程计算程序的组织。自己编写的matlab源代码。-Anderson the computational fluid mechanics and its application "chapter 10 through the flat of supersonic flow section 10.4- navier stokes equation calculation procedure of the organ
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
charpt8_3
- 安德森《计算流体力学及其应用》第八章二维超声速流动的数值解——普朗特—迈耶稀疏波 8.3节 普朗特—迈耶稀疏波流场的数值解。自己写的matalb源代码。-Anderson the computational fluid mechanics and its application "chapter 8 two-dimensional supersonic flow of numerical solution- prandtl- meyer rarefaction wave section 8.3
nozzle-and-diffuser
- 模拟二维可压缩超音速风动内的流动参数随风动形状的变化-Simulate the two-dimensional compressible supersonic wind-driven flow parameters in the wind dynamic changes in shape
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
MeshRefine
- 气体动力学自适应加密程序,用与计算超音速流动。-GKS mesh refinement code for supersonic flow
dahthesis.pdf
- DALE hudsons thesis on simulation of supersonic shear layer using computational fluuid dynamics. This is work done ar penn state univ about decade ago.
Lawaer1
- 准一维,拉瓦尔喷管亚-超声速非守恒型方程求解-Quasi one dimensional, sub- Lawal nozzle supersonic non solution of the conservation equations
Lawaer3
- 准一维,拉瓦尔喷管亚-超声速守恒型方程求解-Quasi one dimensional, sub- Lawal nozzle supersonic conservation equation
