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201.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2023,71(1):176-198
The influence of sudden stratospheric warming (SSW) on the ionosphere and ionospheric irregularities has been studied extensively over the years. However, majority of these investigations have been conducted using warming events originating from the northern hemisphere. Only a few studies have been done on ionospheric variations due to the Antarctic SSW events and to the best of our knowledge, there have not been any studies on southern hemisphere SSW and the occurrence of ionospheric irregularities. In this study, the occurrence of ionospheric irregularities during the 2019 minor Southern hemisphere (SH)/Antarctic SSW is investigated. The event occurs in a relatively calm solar and geomagnetic activity period which makes it possible to identify the effects of SSW on the occurrence of irregularities. Three ionosondes located in different latitudinal regions in Brazil as well as a network of ground-based GPS receiver stations located in both Brazil and Africa were used for this undertaking. Complimentary data from the same ionosonde stations using the same months from 2017 and 2018 were also used. On average more Spread-F was observed in 2019 than in 2017 or 2018 at all stations. ROT observations showed more occurrence in the Brazil sectors followed by West Africa and thenEast Africa. It was observed that the occurrence frequency decreased between 8% and 46 % from the pre-SSW phase to ascending/peak phases and from 2018 to 2019 for the peak phase. 相似文献
202.
针对旋翼干扰下的直升机尾桨气动噪声计算问题,将CFD方法与Farassat 1A(F1A)公式相结合,提出了一种适用于旋翼干扰下的尾桨气动噪声数值计算方法。首先,应用所提出的方法进行了噪声的算例验证,并与参考文献结果进行了对比;然后,着重针对悬停和前飞状态旋翼干扰下的尾桨噪声及气动特性进行了计算分析,并与孤立尾桨状态进行了对比。计算分析结果表明:悬停状态下,旋翼干扰下的尾桨气动噪声水平显著大于孤立尾桨;而在前飞状态,由于旋翼尾迹对尾桨桨盘平面产生更强的气动干扰,这一现象会更加明显;同时,在旋翼干扰作用下,尾桨噪声的主传播方向也会发生明显变化。 相似文献
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就A330飞机F/CTL SENSOR FAULT警告信息在最低设备清单里的条款要求进行说明,通过多角度分析并结合实际工作给出执行建议,并对容易误解之处做出详细说明. 相似文献
205.
针对某型发动机电子控制器,对航空发动机分布式控制系统进行了初步研究。设计了1种基于分布式控制,用AD598、TMS320F2812 DSP和CAN总线构成的航空发动机智能导叶控制装置。阐述了智能导叶控制装置的壳体设计方法,以及TMS320F2812最小系统、基于AD598的LVDT(线性可变差动变压器)信号调理电路、电液伺服阀电流驱动电路(电流输出电路)、CAN总线接口电路和D/A转换模块等电路的设计方法,简述了软件系统设计。通过完成半物理试验,基本满足了对风扇进口可调叶片角度α1、高压压气机进口可调静子叶片角度α2的控制要求。结果表明:该装置具备体积小、智能化程度高、控制效果好等特点。 相似文献
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N.Y. Zaalov H. Rothkaehl A.J. Stocker E.M. Warrington 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
The morphology of the auroral, sub-auroral and mid-latitude trough region of the ionosphere is strongly dependent on the interplanetary magnetic field and the level of geomagnetic activity. Changes in the morphology impact on the characteristics of HF signals propagating through these regions of the ionosphere. In order to develop a better understanding of these effects, a number of experiments have recently been undertaken in which the time of flight and direction of arrival of HF signals have been measured over several paths aligned along the mid-latitude trough. In addition, observations made by the DEMETER satellite of the mid-latitude trough electron density structure, dynamics and wave activity were used in order to investigate the effect of the fine structure of the ionosphere on HF signals. For two types of relatively common night time HF time of flight and azimuth of arrival behaviour (referred to here and elsewhere as ‘Type 1’ and ‘Type 2’ propagation), the signal behaviour is consistent with scatter from irregularities in the auroral region in the one case, and from irregularities present on the floor of the trough in the other. 相似文献
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210.
第四代战斗机的动力装置 总被引:1,自引:0,他引:1
本介绍了国外第四代战斗机对动力装置的要求,归纳了第四代战斗机发动机的主要新技术,分析了第四代战斗机发动机在超声速巡航、可探测性、全寿命费用和发展潜力等方面所具有的优势,最后总结了第四代战斗机发动机发展过程中的几个重要特点,并对发动机技术发展进行了展望。 相似文献