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Aeroelastics_Bifurcation
- 该Matlab程序用于超音速气流作用下板梁的非线性颤振分析-The Matlab program for nonlinear flutter analysis of supersonic airflow plate girder
MOC_NOzzle3D
- computer program for the calculation of steady three dimensional adiabatic flows in supersonic rocket engine nozzles. The fluid is assumed to be an inviscid perfect gas and the flow is assumed to be shock free. The governing equations for this flow m
w12sc3
- W12SC3是美国基于USSAERO程序的超声速机翼设计及分析代码，可用于机翼的整个设计、分析及优化过程。-W12SC3- Supersonic wing design and analysis using source and vortex panel singularity distributions, based on the USSAERO program by Woodward. W12SC3 combines source and vortex panel singulari
NS
- 平板上的超声速流动：完整的纳维-斯托克斯方程的数值求解-Supersonic flow on the plate: full Navier- Stokes equations Numerical Solution
Step
- CFD计算：用于计算超声速前台阶流动C语言程序，生成每一个网格点的密度、马赫数等数据-CFD calculation: used to calculate the supersonic front step flow in C language, generate each grid point density, Mach number and other data
2
- EFFECTS OF UPPER-SURFACE BLOWING AND THRUST VECTORING ON LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE SUPERSONIC TRANSPORT MODEL
3
- EFFECTS OF UPPER-SURFACE BLOWING A N D THRUST VECTORING ON LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE SUPERSONIC TRANSPORT MODEL
CFD-10
- 对应计算流体力学基础及应用中第8章中的例子，有助于读者学习超声速外略平板流动中流场的分布，为深入学习计算流体力学打下坚实的基础(Corresponding to the basis of computational fluid dynamics and the examples in the eighth chapter, it will help readers to study the flow field distribution in supersonic flow in a sligh
Chapter9_Version_3
- 计算流体力学基础及应用第9章，非本人编写。超音速平板绕流数值计算程序(Computational fluid dynamincs. JohnD. Anderson Chapter9_Version_3 supersonic flow over flat plate code)
fpCPU
- 计算流体力学入门超声速平板流动，采用MACCORMACK法时间推进求解(Calculation of supersonic flat plate flow in fluid mechanics)
可压缩准一维管道无粘流动-欧拉方程-MacCormack
- 本题利用一维欧拉方程求解可压缩一维无粘管道流动，并针对出口不同的条件，出口亚音速和出口超音速两种不同条件，将流道进行网格划分，利用MacCormack进行差分求解，得到管道内的总压、马赫数、总焓、内能的分布，并给出计算过程中残差收敛的过程。(A one-dimensional Euler equation is used to solve the compressible one-dimensional viscous pipe flow, and the flow channel is mes
featool-multiphysics-1.9-0
- MATLAB toolbox, 用于简单的流体动力学和热传导模拟仿真(FEATool 1.9 features two new pre-defined physics modes for flow simulations. The new compressible Euler equations physics mode allows for modeling of inviscid and supersonic fluid flows with shock-waves. In addition
NozzleDesign-master
- NASA的超声速喷管设计程序，包含有气体数据库，功能强大(NASA's supersonic nozzle design program, including a gas database, is powerful)
ablation
- 用于计算高超音速飞行器再入大气层的表面烧蚀热化学反应计算(CALCULATION OF THERMOCHEMICAL REACTION OF SURFACE ABRACTION FOR REENTRY OF HIGH SUPERSONIC VEHICLES)