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GridGeneration
- 二维圆钝体高超声速绕流，适用高超声速研究参考用-Two-dimensional hypersonic blunt body flow around a reference for hypersonic research
nseg
- NSEG是美国兰利研究中心推出的飞行器起飞、爬升、巡航、加速、下降、减速和着陆等各个过程分析软件。-NSEG was developed to perform rapid aircraft mission analyses. It is based upon the use of approximate equations of motion whose form varies with the type of flight segment. Flight segments consid
1-An-Integrated-Approach-to-Hypersonic
- 1-An Integrated Approach to Hypersonic
DSMC3
- 稀薄流情况下用蒙特卡洛法计算高超音速的三维程序-Rarefied hypersonic flow case of calculating the three-dimensional program with the Monte Carlo method
DSMC2
- 稀薄流情况下用蒙特卡洛法计算高超音速的二维程序-Monte Carlo method to calculate hypersonic rarefied flows under the two-dimensional case program
DSMC0D
- 稀薄流情况下用蒙特卡洛法计算高超音速的一维程序-Under current condition computing hypersonic rarefied one-dimensional program by Monte Carlo Method
DSMC0R
- 稀薄流情况下用蒙特卡洛法计算高超音速的一维程序-Under current condition computing hypersonic rarefied one-dimensional program by Monte Carlo Method
DSMC-2Dcylinder-master
- 采用粒子算法，模拟高超声速圆柱绕流，得到温度场与速度场等(The particle algorithm is used to simulate the hypersonic flow around a cylinder, and the temperature and velocity fields are obtained.)
Clear
- 通用高超声速飞行器纵向模型为研究对象，并针对线性化模型，分别采用极点配置、LQR以及 三种方法设计控制器以改善系统的性能。(The general hypersonic vehicle longitudinal model is the research object. Aiming at the linearized model, pole placement, LQR and three methods are used to design the controller to improve
hypersonic
- 研究高超声速飞行器的可以看一下，很全面的总结和概括(For the research of hypersonic vehicle, we can see a comprehensive summary)