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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
vlmd
- 计算低速气动力的涡格法程序,来自NASA,可信度高-This is a vortex lattice aerodynamic program from the low speed aerodynamics group at NASA Langley
VLMpc
- Vortex lattice analysis and design: VLMpc-John Lamar s two surface vortex lattice program, developed at NASA Langley. The program treats two lifting surfaces using up to 200 panels. Vortex flows are estimated using the leading edge suction analogy. T
mK
- 蒙克卡罗 蒙特·卡罗方法(Monte Carlo method),也称统计模拟方法,是二十世纪四十年代中期由于科学技术的发展和电子计算机的发明,而被提出的一种以概率统计理论为指导的一类非常重要的数值计算方法。是指使用随机数(或更常见的伪随机数)来解决很多计算问题的方法。与它对应的是确定性算法。蒙特·卡罗方法在金融工程学,宏观经济学,计算物理学(如粒子输运计算、量子热力学计算、空气动力学计算)等领域应用广泛。-蒙克卡罗蒙 Carlo method (Monte Carlo method), als
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- Paper on effect of wing edge deflection on low speed aerodynamic characterisitics.
MagnusEffectLiftAirfoi20150410066.pdf
- We present this paper as an experimental study of employing Magnus Effect in an aircraft wing. The scope and interest of study of Magnus Effect and its application in Aerospace Engineering is widely increasing all over the world to make use of the