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In this paper, the direct simulation Monte Carlo method is employed to simulate flows of modeled air vehicles having simple geometric shape such as delta wing at a Knudsen number between 0.001 and 0.1 for various Mach number and angle of attack conditions. With the calculated aerodynamic forces and heating, we obtained the general behavior of the rarefied gas effects on the vehicles' aerodynamics.

本文采用直接模拟 Monte Carlo 方法,模拟了简单外型如三角翼形的模型飞行器在努森数为 0.001到 0.1的范围内以不同来流马赫数和不同飞行攻角飞行时的流场,计算了飞行器所受到的气动力和气动热,获得了稀薄气体效应对飞行器气动性能影响的一般规律。

The results show the high accuracy quality of spectral element method and the stability of Newmark time integral method. Then some computational parameter is changed in example one such as the subdivision style of computational domain, time step length and such on. Some important conclusions and strategies for spectral element method with Newmark integral method for computational aeroacoustics can be given. The feasibility of spectral element method for computational aeroacoustics is verified.

计算结果表明谱元方法的高精度及Newmark时间积分方法的稳定性,并改变算例的计算参数,例如计算区域剖分方式、时间推进步长等进行了计算,得出了一些重要结论,为使用谱元方法结合Newmark积分求解气动声学问题积累了重要的经验,最终证明了谱元方法求解计算气动声学问题的可行性。

The five methods are tested on a 2-D test function ,a straight airfoil and a sweepback airfoil. For the straight airfoil,the paper constructs its approximation models of structure disciplinary, aerodynamic disciplinary and stealth disciplinary.

用这五种方法分别构造二维测试函数的近似模型,直机翼结构学科、气动学科和隐身学科的近似模型和后掠机翼结构学科、气动学科的近似模型,并总结这五种方法对二维测试函数、直机翼和后掠机翼各学科近似的适用性。

My main research work is listed as follows: 1. Considering structure characteristics of high aspect ratio flexible wing, features of flat-straight-wing and backswept wing, the aeroelasticity of high aspect ratio of flexible wing, its structure model and aeroelastic dynamics equation of flexible wing have been studied.

针对大展弦比柔性机翼的结构特征,并考虑到平直机翼和后掠机翼的特点,对大展弦比机翼的气动弹性进行分析,分别建立其结构模型,并推导出柔性机翼气动弹性的动力学方程。

The results show that, for the first with no headwall, when there is no crosswind, it has small front face areas, so the aerodynamic resistance is the least. Since the second and the third have headwall, the front face areas are large, so they have bigger aerodynamic resistance. Under the condition of crosswind, as the third design option has the highest side beam, the area of positive pressure at the upwind is bigger, and the area of negative pressure is smaller when the bigger eddy area appears, so the side forces become larger. The first has the least side forces; the overturning moment of the first is the least.

研究结果表明:在无横风情况下,方案一中没有端墙,迎风面积较小,受到的气动阻力最小,方案二和三中平车有端墙,迎风面积较大,受到的气动阻力也较大;有横风情况下,方案三中平车侧梁较高,车体迎风面正压区较大,而背风侧产生较大的涡流区,在此区域内压力较小,故其横向力较大,方案一中平车侧梁没有加高,受到的横向力最小;方案一中平车倾覆力矩最小,稳定性最好。

Based on the literatures about the study of micropumps in uTAS for these years, this thesis brought forward a novel approach for microfabrication of modified pneumatic microvalves on microfluidic chips using glass-PDMS bonding technique. And then we studied on the factors that may influence the capability of microvalves.

本文在对近几年来μTAS领域有关微泵的研究报道进行综述的基础上,研究制备了一种用于微流控芯片的改进型玻璃—PDMS气动致动微阀,并对气动微阀的性能进行了考察。

Although they used the 3D modes of the deck in the determination of aerodynamic characters so that the mechanical coupling and aero-coupling between the modes can be depicted more correctly ; in order to reduce the computation effort, however, they still adopted the partial differential equation to characterize the buffeting motion of the deck modeled as a uniform beam.

尽管他们将桥面的三维振型应用于计算气动特性分析中,从而可以较真实地描述振型间的机械和气动耦合。但是为了减小计算规模,他们仍然是用均匀梁的偏微分方程来描述桥面的抖振运动。

The characteristics of the inner flow field and outer sound field of a pneumatic valve sound generator is analyzed with its theoretical model,numerical simulation and experimental results.

在对气动阀门发声器的工作过程进行描述基础上,通过理论分析和数值计算与实验相结合的方法,分析了气动阀门发声器的内部流场和外部声场的特征。

We produce kinds of Air Cylinder, Direction Control Valve, Gas Generator and etc. with nice sculpt, complete specification, good function and reasonable structure. It's suitable for oil field, textile industry, machinery, electronics industry and etc. It's an ideal product to replace manual operations.

我厂生产的各种气缸、方向控制阀、气源处理件、气动辅助等各类气动产品,品种繁多,规格齐全、外型美观、结构合理、性能优良,该产品适用于油田、纺织、机械、电子等行业的流水线生产,是替代烦琐的手工操作从而达到提速的理想产品之一。

So in this paper, the micro-turbofan engine, which has several ten kilogram thrust level, moderate difficulty, low pressure ratio and single rotor, is studied in three ways which contain overall aerodynamics arrangement analysis and structure feasibility research, optimizing of aerothermodynamics circulation, overall aerodynamics design ane flying performance simulation.

本文对于数十公斤推力量级的、工程技术难度适中的、低增压比的一种单叶轮微型涡扇发动机,进行了总体气动布局分析和结构可行性研究,热力循环优化设计,总体气动设计及飞行特性模拟这三个方面的研究。

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