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351.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(1):115-128
The ionospheric effects induced by the September 2017 storm have been exceptional compared to other events in the solar cycle 24. This paper gathers results of the ionospheric observations at the European middle latitude station Pruhonice. It consists of evaluation of ionospheric vertical and oblique sounding, Digisonde drift measurement, and data obtained from the Continuous Doppler Sounding System. We observed strong ionospheric response with an unusual stratification of ionospheric layers, Large Scale Traveling ionospheric disturbances, changes in electron density, and increase and oscillations in plasma drift velocity. 相似文献
352.
Rosario PECORA 《中国航空学报》2021,34(7):13-28
Morphing wing structures are widely considered among the most promising technologies for the improvement of aerodynamic performances in large civil aircraft. The controlled adaptation of the wing shape to external operative conditions naturally enables the maximization of aircraft aerodynamic efficiency, with positive fallouts on the amount of fuel burned and pollutant emissions. The benefits brought by morphing wings at aircraft level are accompanied by the criticalities of the enabling technologies, mainly involving weight penalties, overconsumption of electrical power, and safety issues. The attempt to solve such criticalities passes through the development of novel design approaches, ensuring the consolidation of reliable structural solutions that are adequately mature for certification and in-flight operations. In this work, the development phases of a multimodal camber morphing wing flap, tailored for large civil aircraft applications, are outlined with specific reference to the activities addressed by the author in the framework of the Clean Sky program.The flap is morphed according to target shapes depending on aircraft flight conditions and defined to enhance high-lift performances during takeoff and landing, as well as wing aerodynamic efficiency during cruise. An innovative system based on finger-like robotic ribs driven by electromechanical actuators is proposed as morphing-enabling technology; the maturation process of the device is then traced from the proof of concept to the consolidation of a true-scale demonstrator for pre-flight ground validation tests. A step-by-step approach involving the design and testing of intermediate demonstrators is then carried out to show the compliance of the adaptive system with industrial standards and safety requirements. The technical issues encountered during the development of each intermediate demonstrator are critically analyzed, and justifications are provided for all the adopted engineering solutions. Finally, the layout of the true-scale demonstrator is presented, with emphasis on the architectural strengths, enabling the forthcoming validation in real operative conditions. 相似文献
353.
354.
采用大涡模拟,考察了旋转影响气膜冷却的物理机制。参考实验模型,用带有30°倾斜圆柱孔的平板模拟涡轮转子叶片的吸力面,冷气出口雷诺数为1300,冷气和主流的吹风比为0.5,计算了静止和旋转数为0.2两种条件下的流动和换热,全面展示了旋转对平均流场、涡量、湍流结构和壁面温度分布的影响,并由此对实验现象进行了解释。结果表明,旋转使气膜孔下游的对转涡对产生不对称性;旋转引发的哥氏力使气膜冷却流场中的发夹型漩涡结构向高半径方向偏移,引起涡量分布的改变;旋转破坏了发夹涡的连续性,减少了对主流的卷吸和主流传递给冷气的热量,从而提高了冷却核心区的冷却效率,与实验中观察到的现象一致。 相似文献
355.
《中国航空学报》2021,34(5):364-372
In order to understand the physical phenomenon of the reflected shock/turbulent boundary layer interaction, the Large Eddy Simulation (LES) is conducted to investigate shock wave and turbulent boundary layer interaction in a compression ramp with inlet high Mach number of 2.9. Rescaling/recycling method is used as inflow turbulence generation technique and validated on a supersonic flat plate turbulent boundary layer. The flow field of recycling plane in the plate computation domain is obtained to give the inlet boundary condition for the LES computation. This paper focuses on the reflected shock/turbulent boundary layer interaction region, where the fine flow structure and instantaneous flow field are analyzed in detail. It is found that the unsteady motion of the shock wave leads to the increase of wall pressure fluctuation. 相似文献
356.
文章主要推导了可用于描述大型降落伞绳帆和抽打现象的一般绳索三维动力学连续模型,及弦坐标系下可用于求解绳帆现象的两点边值问题(BVP)模型,并采用某型号大型降落伞的空投录像和杆件算例对模型进行验证对比,说明了模型的正确性,采用这一连续模型能够更直观地对大型伞的绳帆和抽打现象进行定性和定量分析。 相似文献
357.
入口利用层流速度型叠加二维和三维Tollmien-Schliting(T-S)波,应用动态亚格子模型、预处理技术以及高精度算法,采用大涡模拟(Large eddy simulation,LES)数值计算方法,对可压缩平板边界层空间模式的转捩机理及其拟序结构进行了研究。计算结果展示了T-S波经历线性、非线性发展阶段破碎形成发卡涡,最终演化成具有4个涡环的涡链结构的整个过程,并揭示了发卡涡涡腿并非完整对称及低速条带在涡环产生的位置不连续的现象,探讨了主流向涡与壁面相互作用诱导生成次流向涡的机理。 相似文献
358.
Jorge A. Pérez-Peraza Eduard V. Vashenyuk Apolonio Gallegos-Cruz Yurii V. Balabin Leonty I. Miroshnichenko 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(6):947-954
Based on the concept of multiple acceleration of solar energetic particles (SEP) we analyzed the super-event of 20 January 2005 by the data of ground level, balloon and spacecraft observations. The main characteristics of relativistic solar protons (energy spectra, anisotropy directions and pitch-angle distributions) are derived and their dynamics during the event is studied. It is shown that the flux of relativistic solar protons may consist of two distinct components, the so-called prompt and delayed ones. Within a two-source model of particle generation, one of which is associated with an expanding magnetic loop, we solved the transport equation in energy phase space, including adiabatic losses simultaneously with the stochastic acceleration process, and calculate the expected spectra of the delayed component at the source. The confrontation of experimental spectra with theoretical ones shows that the delayed component may be correctly described by stochastic acceleration, but not the prompt component. The required acceleration efficiencies turned out to be rather high, so that, for this particular event, adiabatic cooling is practically negligible. Our results provide a new support to the existence of two populations of relativistic solar protons in some SEP events. 相似文献
359.
采用0.3 MPa压力对DD6单晶高温合金进行水吹砂,然后用电子束物理气相沉积的方法在DD6合金基体上制备了热障涂层,将带热障涂层试样置于1100℃空气气氛中分别进行50 h和100 h热暴露,在1100℃/130 MPa条件下测试持久性能。研究了水吹砂及高温热暴露对带热障涂层DD6合金组织的影响。结果表明:0.3 MPa压力水吹砂制备热障涂层并高温热暴露后没有发现再结晶组织;热暴露过程中,基体和涂层之间的元素会发生不同程度的互扩散;表面残余应力和元素互扩散导致了γ′相粗化方向的变化;性能测试后试样断口附近的涂层与基体界面下方局部区域形成了二次反应区。 相似文献
360.
介绍了美国NI公司的数据采集板PC—DIO—96的功能,及其在Windows95下软硬件的安装,描述了如何使用其随板软件包,并给出了其三种主要功能(线功能、口功能和组功能)的程序框图。详细介绍了在“建立大尺寸计量标准”题目中应用该板进行环境参数的采集和电机控制。 相似文献