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aerodynamic相关的网络例句

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与 aerodynamic 相关的网络例句 [注:此内容来源于网络,仅供参考]

In order to apply neural network and intelligent control in supermaneuverable flight, the mathematic model of flighter is obtained, and the nonlinear aerodynamic coefficients are identified using computational neural networks, then, a neural network control system for supermaneuver is designed according to the timescale, and a intelligent compensator is givento compensate for the system errors which are caused by the networks training error, no-samples input, disturbance and time-delay, etc, which including the design of knowledge base, blackboard and reasoning engneer, the simulation results of Herbst maneuver demonstrate the designed control system is satisfying.

为了在超机动中应用神经网络和智能控制,本文接着建立了超机动时飞机的数学模型,并利用神经网络对大迎角下非线性非定常气动力进行了辨识建模,然后按时标分离法设计了一个针对超机动飞行的神经网络控制系统。

Considering the presence of large aerodynamic uncertainties in the process of flighting for launch vehicle and resilience vibration, liquid propellant rocking have a certain infulence on system, the design method of H〓 robust control systems with parameter uncertainties and unmodelled dynamics is researched.

首次对同时存在系统矩阵、控制输入矩阵的不确定和系统关联不确定变化以及有界能量干扰的关联大系统提出了一种简便的局部状态反馈分散H〓控制器的设计方法。

In airplane design, structural nonlinearities cannot be avoided. The structuralnonlinearities arise from worn hinges of control surfaces, loose control linkages,material behavior and various other sources. In the flighting, the aerodynamicnonlinearities also cannot be avoided. The aerodynamic nonlinearities can benegligible when the speed of the plan is not very high;but when the speed of the planis supersonic or highly supersonic, it cannot be negligible.

在飞机设计中,结构非线性是不可避免的,结构非线性源于控制其表面的旧铰链,松散的控制器联动装置,材料性能和其它的来源;在飞机的飞行中,气动的非线性也是不可避免的,对于飞行速度不是很高的情况,气动的非线性是可以忽略的,而对于超音速以及超高音速的飞机来说,气动的非线性是不可以忽略的。

Chengdu major service centre for the southwest, northwest regional sales agents of the Company of Germany BECKER, France LEYBOLD, Germany BUSCH, Germany SIEMENS, the United States GAST, Japan FUJI, Taiwan CRELEC, and other famous brands, these brands are in the field of aerodynamic technology in the global Leadership position, and its products widely used in electronic, chemical, medical, food packaging, printing, shoe machinery manufacturing, metal washing, vacuum from plastic foam, sewage treatment and other industries.

成都服务中心主要面向西南、西北地区销售本公司代理的德国BECKER、法国LEYBOLD、德国BUSCH、德国SIEMENS、美国GAST、日本FUJI、台湾CRELEC等著名品牌,这些品牌在气动技术领域皆处于全球性领导地位,其产品广泛地应用于电子、化学、医疗、食品包装、印刷、鞋类机械制造、金属洗濯、塑料真空脱泡、污水处理等行业。

Based on 3D steady and incompressible N-S equation and k-ε turbulent model, the aerodynamic performance of three different design options of 160 km/h container flat wagon was analyzed and compared using finite volume method. The three design options are as follows: the first design option has no headwall and the side surface of side beam is flat; the second and the third both have headwall and high side beam, and the side surface of side beam of the second is obtuse, while the third is cambered.

基于三维、不可压、定常N-S方程和k-ε双方程湍流模型,采用有限体积法对3种不同设计方案在运行时速为160 km/h的集装箱专用平车在有、无横风情况下的气动性能进行分析与比较,其中:方案一的平车无端墙,侧梁侧面平直;方案二和三的平车均加有端墙,且侧梁加高、侧面形状分别为钝形和弧形。

Based on 3D steady and incompressible NS equation and kε turbulent model, the aerodynamic performance of three different design options of 160 km/h container flat wagon was analyzed and compared using finite volume method. The three design options are as follows: the first design option has no headwall and the side surface of side beam is flat; the second and the third both have headwall and high side beam, and the side surface of side beam of the second is obtuse, while the third is cambered.

摘 要:基于三维、不可压、定常 N S 方程和 k ε双方程湍流模型,采用有限体积法对3种不同设计方案在运行时速为160 km/h的集装箱专用平车在有、无横风情况下的气动性能进行分析与比较,其中:方案一的平车无端墙,侧梁侧面平直;方案二和三的平车均加有端墙,且侧梁加高、侧面形状分别为钝形和弧形。

Meanwhile some detailed numerical researches are done on the influence to the aerodynamic field throughout changing magnitude of the primary air and the secondary air, adopting homocentric two tangential circles, tangentially-fired in number one and number three corner face-fired in number two and number four corner, changing the air distribution of the secondary air and the reverse swirl of upper secondary air, Which provide the theoretical basis for boiler design, optimal operation, renovation etc.

本文同时应用数值研究方法模拟了四角切圆锅炉一二次风大小变化、大小同心切圆布置方式、一三角相切二四角对冲、二次风配风方式改变、二次风反切等对炉内流场特性的影响,为优化锅炉设计、改造、运行提供了及其有意义的理论上的指导。

Methods AH dry powder inhalation was prepared by spray-drying method. Following spray-drying, resultant powders were characterized using scanning electron microscopy and laser diffraction, and the aerosolisation performance was determined using twin-stage liquid impinger. The process conditions were optimized with orthogonal design combined with multi-index test. The powder yield, aerodynamic diameter, angle of repose and respirable fraction were used as indices for orthogonal design.

采用喷雾干燥法制备盐酸氨溴索干粉吸入剂,采用双层液体碰撞器测定盐酸氨溴索干粉吸入剂体外沉积率,扫描电镜观察粉粒的形态,激光粒度测定仪测定粒径大小,以产品收率、粉末的空气动力学径、休止角及体外沉积率为考察指标,通过正交设计结合多指标综合评价法优化最佳制备工艺。

In this paper,a viscous/inviscid analysis and calculation method is used to analyze the aerodynamic performance of a series of novel airfoils for wind turbine.

风力机翼型气动性能是风力机气动设计和性能分析的重要基础。

The maximum of the L/D appear at about 30-degree angle of attack. The bugle of the reentry module drops the trim angle. Pyrochemistry reaction largen Ca, Cn, diminish L/D and the trim angle. The variational tendency of aerodynamic characters with angle of attack in high altitude (higher than 105km) is different from that of in low altitude (lower than 105km).

返回舱凸出物使配平攻角减小;高温热、化学非平衡效应使轴向力和法向力系数有所增大,升阻比在数值上有所减小,配平攻角略有降低;返回舱0°~180°攻角范围内的气动力特性高空(105km以上)随攻角的变化趋势与低空(105km以下)的变化趋势不同。

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