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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
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
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.
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
quasi_one_dimensional_nozzle
- 麦克马克方法求解一维亚-超声速等熵喷管流动（守恒型）-quasi one dimensional nozzle mccormack subsonic supersonic1
Maccormack
- mac cormak method solving a subsonic converge diverge pipe
MacCormack_shockwave
- Mcmark程序，求解守恒型流动方程，激波捕捉，超声速（亚声速）入口、出口需要自己调节-Mcmark program, Conservative solving flow equations, shock capturing supersonic (subsonic) inlet, an outlet need to regulate their own
5
- SUBSONIC PITCH-UP ALLEVIATION ON A 74 DEG. DELTA WING
TTECTrA
- The tool for turbine engine closed-loop transient analysis (TTECTrA) is a semi-automated control design tool for subsonic aircraft engine simulations. At a specific flight condition, TTECTrA produces a basic controller designed to meet user-defined