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151.
本文从运动气流的二维激波动力学方程组出发,提出了一种计算平面运动激波和尖锥头激波迎面干扰问题的新方法。该方法可以计算穿透激波的强度和形状,马赫反射时三波点的轨迹,马赫杆的强度和几何形状,以及锥面峰值压力的大小。计算结果与数值模拟、其它计算方法以及实验数据进行了比较,结果表明本方法不仅精度较高,而且保持了简捷,省机时的优点。 相似文献
152.
Nonlinear interactions between the quasi 5-day wave and tides based on meteor radar observation in the Mesosphere and Lower Thermosphere(MLT) at Maui are studied in this paper.Strong sum interaction between quasi 5-day wave and diurnal tide,and evident difference interaction between quasi 5-day wave and semidiurnal tide are observed during the time of attention.However,their difference and sum counterparts are clearly weaker.The secondary waves generated from those interactions beat with the tide and show intense modulation at the period of 5 days which confirms the existence of their interactions.Additionally,correlation coefficients among these waves are calculated to further explore their interactions and find that they can persist for several days although they are highly intermittent.The energy exchange among these waves can be reversible during the observational time.The periods when the significant difference interaction between the quasi 5-day wave and semidiurnal tide occur are much shorter than those when the significant sum interaction between the quasi 5-day wave and diurnal tide occur.Moreover,these two strong interactions can take place simultaneously.In generally,this study provides the proof of nonlinear interactions between quasi 5-day wave and tides which were seldom reported before. 相似文献
153.
刘存伟 《中国民航飞行学院学报》2013,(1):66-68
要培养具有英语实际应用能力的学生,提升教学质量,改革现有的大学英语评价制度势在必行。本文提出,大学英语无纸化考试、人机对话、构建完善的课程评价机制,教考分离等方式方法,应该在大学英语教学中得到进一步加强。 相似文献
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155.
Enrico Stoll Jürgen Letschnik Markus Wilde Alvar Saenz-Otero Renuganth Varatharajoo Jordi Artigas 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Orbital robotics focuses on a variety of applications, as e.g. inspection and repair activities, spacecraft construction or orbit corrections. On-Orbit Servicing (OOS) activities have to be closely monitored by operators on ground. A direct contact to the spacecraft in Low Earth Orbit (LEO) is limiting the operational time of the robotic application. Therefore, geostationary satellites are desirable to relay the OOS signals and extend the servicing time window. A geostationary satellite in the communication chain not only introduces additional boundary conditions to the mission but also increases the time delay in the system. The latter is not very critical if the servicer satellite is operating autonomously. However, if the servicer is operating in a supervised control regime with a human in the loop, the increased time delay will have an impact on the operator’s task performance. 相似文献
156.
作为"风扇出口导向叶片(Outlet Guide Vanes,OGV)低噪声设计"系列文章的第1篇,本文在现有压气机气动设计流程的基础上,加入了噪声评估过程,建立了基于通流设计的气动/声学一体化设计方法。为提高设计阶段的评估速度,以三维升力面理论与管道声学理论为基础,从通流设计和造型设计输出中提取参数,结合转子尾迹模型,建立了转/静干涉噪声的解析预测模型。以现代大涵道比涡扇发动机风扇/增压级为对象,采用该模型系统分析了OGV轴向掠形与周向倾斜对转/静干涉噪声的影响,获取了轴向掠形角与周向倾斜角等三维设计参数与风扇噪声的关系图谱,初步确定了低噪声设计较优降噪量的掠和倾组合方案。以此为基础,在保持叶尖子午投影位置和弦长不变的前提下,将叶片前缘和径向积叠进行参数化,采用遗传算法进一步开展了OGV的低噪声优化设计,最终获得了2个优化方案,预估的降噪量达到了8 dB。 相似文献
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158.
Wind tunnel evaluation of the aerodynamic interaction effects between plume and the external flow past the missile body including the wake boundary (“slipstream”) over powered flight envelopes of rocket propelled vehicles can be greatly facilitated — or even made possible — by a methodology replacing the hot propellant by cold, inert gases. Model nozzle design is based on the second order matching of plume geometry and first order modeling of plume stiffness. Since modeled nozzles will have larger throat radii than the prototypes, one can use sting-supported, sting-fed model installations thus eliminating aerodynamic interference effects due to struts. The concepts of simulated altitude and simulated full-scale Reynolds Number greatly reduce wind tunnel occupancy time. Computer programs, covering all steps of evaluating prototype nozzle performance, model sting nozzle design, model test evaluation and interpretation have been developed. The modeling methodology is supported by experimental results obtained in an induction wind tunnel at the FFA, Bromma, Sweden and in the 16 T and VKF-A altitude tunnels at AEDC, Tullahoma, Tenn. 相似文献
159.
Anpredictionsystemforthein-ductsoundfieldinaeroenginecanprovidethetheoreticalfoundationforthepracticalengineeringsup-pressing... 相似文献
160.
叶片弯掠组合设计对风扇气动噪声的被动控制 总被引:1,自引:2,他引:1
转子尾迹与静子叶片干涉是产生风扇离散噪声的主要噪声源之一。环形叶栅几何对于声源项的求解以及管道内的声传播都有重要影响,因此在讨论叶片弯掠组合设计对于风扇噪声的被动控制作用时需要重点强调三维效应的影响。本文利用三维升力面理论,建立了可以考虑叶片弯掠组合影响的气动声学模型。相比数值计算方法,三维升力面理论不存在频散耗散影响,求解快速高效,更加有利于初始阶段的优化设计,以及为数值计算模型提供验证。通过与已有结果的对比,进一步阐述了叶片后掠和周向倾斜对于风扇离散噪声的影响机制。而弯掠组合设计算例的计算结果表明,在某些条件下,选取合适的叶片弯掠造型能够获得很好的降噪效果。由于轴向传播波数的影响,前传声场和后传声场对于弯掠组合的变化趋势存在一定的差异性。 相似文献