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431.
The preliminary phase is significant during the whole design process of a large airplane because of its enormous potential in enhancing the overall performance. However, classical sequential designs can hardly adapt to modern airplanes, due to their repeated iterations, long periods, and massive computational burdens. Multidisciplinary analysis and optimization demonstrates the capability to tackle such complex design issues. In this paper, an integrated optimization method for the preliminary design of a large airplane is proposed, accounting for aerodynamics, structure, and stability. Aeroelastic responses are computed by a rapid three-dimensional flight load analysis method combining the high-order panel method and the structural elasticity correction. The flow field is determined by the viscous/inviscid iteration method, and the cruise stability is evaluated by the linear small-disturbance theory. Parametric optimization is carried out using genetic algorithm to seek the minimal weight of a simplified plate-beam wing structure in the cruise trim condition subject to aeroelastic, aerodynamic, and stability constraints, and the optimal wing geometry shape, front/rear spar positions, and structural sizes are obtained simultaneously. To reduce the computational burden of the static aeroelasticity analysis in the optimization process, the Kriging method is employed to predict aerodynamic influence coefficient matrices of different aerodynamic shapes. The multidisciplinary analyses guarantee computational accuracy and efficiency, and the integrated optimization considers the coupling effect sufficiently between different disciplines to improve the overall performance, avoiding the limitations of sequential approaches utilized currently. 相似文献
432.
随着现代社会的发展,信息需求量快速增长,低频段频谱资源逐渐耗尽,无线通信频谱开始向着太赫兹波段(0.1 THz~10 THz)拓展,太赫兹通信技术已然成为未来大容量通信的重要发展方向之一。围绕着太赫兹通信技术,介绍了太赫兹通信特点及其应用场景,太赫兹通信用核心元器件的发展,国内外现有成果对比以及未来可能的发展趋势。同时,分别对微波光子学太赫兹通信系统、全固态太赫兹混频通信系统和直接调制太赫兹通信系统三种不同架构的系统进行分析和讨论,并对太赫兹通信技术的发展趋势以及未来应用场景进行了探讨。 相似文献
433.
Swastika Chakraborty Madhura Chakraborty Saurabh Das 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(12):4043-4053
Some second order rain attenuation statistics such as fade duration and fade slope are investigated on the basis of experimental measurements of received signals using the GSAT-14 satellite beacon signal at 20.2 GHz for three years (2014–2016) over the tropical location Ahmedabad (23.02 0E, 72.510N), India with an Elevation angle of 630. Existing models of fade duration are compared with experimental data in this study and exponent of power law model of fade duration at Ka band is further explored. A new model for fade duration for Ka band for tropical locations is proposed where the constant of exponent of attenuation in the power law is found to be 0.143 instead of 0.055 used in ITU-R. Other relevant parameters for implementation of fade mitigation technique to prevent the link outage like cumulative distribution of signal fade rate, maximum and minimum fade rise and fade fall are also studied. Fade slope asymmetry over tropical region is also investigated. Keeping in view of exploiting the commercial launch of Ka band in Indian region there is an urgent need for validation of the existing models of fade slope (specially looking into fade symmetry) and fade duration. It will help the SATCOM (Satellite Communication) link designer to improve closed loop fade mitigation technique to minimize the possible link failure/link outage over the tropical region. 相似文献
434.
雷凌航 《中国民航飞行学院学报》2013,(1):77-80
2011中国民航十大热点事件网络票选中,“国内首架A380交付南方航空公司”排名榜首。南航围绕A380首飞进行的一系列市场策划与公关营销,获得了产品经济效益与品牌美誉度的双赢,被业界称为“一架飞机引发的公关大案”。分析此次产品营销中南方航空的营销策略,对国内航空公司市场理念的拓展,品牌实力的建设,有着积极的启示意义与实践价值。 相似文献
435.
研究了一种利用捷联惯导、星敏感器和北斗接收机进行长航时高精度组合导航的方法.对捷联惯导系统误差、星敏感器安装误差、北斗定位误差分别进行建模,将星敏感器输出的载体姿态角、北斗接收机输出的载体位置与捷联惯导输出的对应参数分别相减作为量测,推导获得组合导航量测方程.针对长航时环境下可能面临量测噪声统计特性的不确定问题,采用简化的Sage-Husa自适应滤波算法进行组合导航滤波设计.仿真结果表明,该组合导航方法的定位精度达到±11.86m,定姿精度达到±0.27′,并且对量测噪声统计特性的突变具有较强的鲁棒性. 相似文献
436.
437.
438.
《中国航空学报》2022,35(9):366-378
Under-race lubrication applied to the inter-shaft bearing of aeroengine is characterized by spray oil collection and oil delivery to the bearing via flow-path structure. Droplet splashing induced by the collision between spray oil and the scoop as well as oil flowing characteristics in the flow-path influence bearing lubrication efficiency. In previous investigations, the spray oil collection and oil delivery analysis were separated, and the effect of droplet splashing on bearing lubrication efficiency was not considered. Moreover, time-varying characteristics of oil delivered to the bearing were not accounted for. This is caused by time variations of the circumferential position of rollers and under-race feed holes. To overcome these limitations, a numerical model which integrates the spray oil collection and oil delivery analysis is proposed in this paper. The model is embedded with the function of calculating the flow rate of splashing droplets and analyzing time-varying characteristics of the oil fed to the bearing. Furthermore, the numerical model is validated by experimental investigation. The proposed numerical model facilitates the accurate calculation of bearing lubrication efficiency as well as the design of an efficient lubrication structure. 相似文献
439.
440.
设计了一种基于绝缘体上铌酸锂(LNOI)的片上多模干涉(MMI)波导功率分束器,在5μm×45μm的小尺上实现了1×2的片上分束功能,且满足集成化光纤陀螺的光路应用要求。通过理论公式和有限时域差分法对器件进行了关键参数计算和光场仿真,MMI干涉区长度为20μm,优化输出分支间距并增加宽度为1.7μm的锥型波导后,在100nm的光谱宽度中,功率分束器的归一化输出光强较为平坦,最低规一化输出光强为0.965,两输出分支的光功率不均匀度仅为10量级。 相似文献