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71.
利用1992年10月27日耀斑极为完整的高质量观测资料,通过对可见光、软X射线和硬X射线图像和光谱的综合分析,诊断耀斑过程中的热与非热性质,结果表明,在这个事件中,热与非热过程并存且在时空演化上呈现不同的特征  相似文献   
72.
Input data of the system are two-dimensional images and one-dimensional distributions of total and polarized solar emission at 5.2 cm wavelength obtained with SSRT. Together with photoheliograms, magnetograms, Hα-filtergrams and characteristics of active regions received from other sources, they form the initial database. The first stage includes superimposing the images, identifying microwave sources with active regions, assigning NOAA numbers to the sources, and determining for each active region the heliolatitude, extent, and inclination angle of the group's axis to the equator. These data are used to calculate the boundaries of longitude zones for each active region. A next stage involves determining the brightness temperatures of microwave sources less than the polarization distribution, the degree of polarization, and microwave emission flux, as well as calculating the parameters of microwave sources. Each parameter is assigned its own value of the weight factor, and the sum of values is used to draw the conclusion about the flare occurrence probability in each active region and on the Sun in general.   相似文献   
73.
Experimental Study on Emission Performance of an LPP/TVC   总被引:2,自引:0,他引:2  
A key issue in the commercial aircraft engine design is environmental acceptability, and designers are continually challenged to reduce emissions. In this paper, an experimental investigation is performed to evaluate the emission performance of a liquid-fueled trapped vortex combustor (TVC) under lean premixed prevaporized (LPP) mode. When operating as an LPP system, a TVC is fueled both in the cavities and in the main stream. The correlations between the emission performance and the total excess air ratio, the positions (4 positions) of the fuel injectors in the main stream, and the inlet temperature are obtained. Experi- mental results show that both the volume concentrations of unburnt hydrocarbon (UHC) and NOx (NO, NO2 usually grouped together as NOx) increase with the increase of total excess air ratio from 1.5 to 3.0; the emission performance relies heavily on the position of the main stream injector, and the best performance is achieved at Position 4 in the experiments; the increase of the inlet temperature impacts on the emission performance positively; the smallest volume concentrations of UHC and NOx obtained in the experiment are 94×10 6 and 2.3×10 6 respectively. This paper validates the feasibility of low emissions for an LPP/TVC and provides a reference for further optimization of TVCs.  相似文献   
74.
    
声发射(AE)技术是一种无损检测方法,可以对飞行器中复合材料结构的动态缺陷进行监测。针对AE信号模态成分复杂以及复合材料各向异性导致源定位精度不高的问题,提出基于经验小波变换(EWT)的广义互相关(GCC)时差定位(TDOA)算法。通过EWT对传感器观测到的AE信号进行自适应的分解重构得到其主频模态,有效提高了各通道信号间的相关系数;通过多向波速测量实验对波速进行了多项式拟合;采用GCC法求取各通道信号的时差对AE源进行定位。在平台实验中以T800型碳纤维复合材料板为对象,以断铅信号为AE源对算法进行了验证,实验结果证明了算法的准确性和实用性。  相似文献   
75.
以一台四缸四冲程压燃式航空煤油活塞发动机为研究机型,运用工程系统高级建模和仿真平台软件(AMESim)仿真软件建立了发动机的整机模型,并使用台架实验的采集数据对该仿真模型进行了验证。在高空环境中,仿真分析了飞行器起飞工况、最大巡航工况下发动机喷油器的不同喷孔数、孔径对发动机燃烧过程、性能和NOx排放特性的影响。计算结果表明:稳态工况下,随着喷孔数的增加,最高燃烧压力和温度增加,瞬时放热率增长速度快且峰值上升;同时,缸内预混燃烧得到强化,燃烧始点提前,滞燃期和燃烧持续期缩短,燃烧重心前移,循环热效率增高,但同时会提高NOx的生成量;在飞行器瞬态变海拔的起飞工况下,多喷孔数、小孔径的喷油嘴有利于航空活塞发动机在高空环境下恢复发动机功率,提升飞行器的动力性和续航性能。   相似文献   
76.
Active region NOAA 11158 produced many flares during its disk passage. At least two of these flares can be considered as homologous: the C6.6 flare at 06:51 UT and C9.4 flare at 12:41 UT on February 14, 2011. Both flares occurred at the same location (eastern edge of the active region) and have a similar decay of the GOES soft X-ray light curve. The associated coronal mass ejections (CMEs) were slow (334 and 337 km/s) and of similar apparent widths (43° and 44°), but they had different radio signatures. The second event was associated with a metric type II burst while the first one was not. The COR1 coronagraphs on board the STEREO spacecraft clearly show that the second CME propagated into the preceding CME that occurred 50 min before. These observations suggest that CME–CME interaction might be a key process in exciting the type II radio emission by slow CMEs.  相似文献   
77.
Quasars are the most luminous sources in the Universe. They are currently observed out to redshift z≈7z7 when the Universe was less than one tenth of its present age. Since their discovery 50 years ago astronomers have dreamed of using them as standard candles. Unfortunately quasars cover a very large range (8 dex) of luminosity making them far from standard. We briefly review several methods that can potentially exploit quasars properties and allow us to obtain useful constraints on principal cosmological parameters. Using our 4D Eigenvector 1 formalism we have found a way to effectively isolate quasars radiating near the Eddington limit. If the Eddington ratio is known, under several assumptions it is possible to derive distance independent luminosities. We discuss the main statistical and systematic errors involved, and whether these “standard Eddington candles” can be actually used to constrain cosmological models.  相似文献   
78.
基于声发射的单层铝板高速撞击损伤类型识别   总被引:1,自引:0,他引:1  
针对基于声发射技术的在轨航天器遭受空间碎片撞击损伤的评估问题,采用AUTODYN软件进行了弹丸超高速正撞击铝板所产生声发射波动信号的数值模拟,给出了二维模拟结果;对所得到的声发射信号进行小波重构,得到低频和高频部分的信号。通过研究低频和高频信号的峰值变化,发现第一和第二峰值幅度与撞击速度的变化具有一定的规律性,通过低频第二峰值幅度与第一峰值幅度比值将高速撞击损伤模式分为成坑、锥形穿孔和圆柱形穿孔三种类型。
  相似文献   
79.
CMEs (Coronal Mass Ejections) are an important means of energy release in the solar corona. Solar Polar Orbit Radio Telescope (SPORT) is a mission being proposed for observing the propagation of interplanetary CMEs from solar polar orbit. The main payload onboard SPORT is a synthetic aperture interferometric radiometer, which receives radio emission of interplanetary CMEs. It is identified that there are mainly three radio emission mechanisms of CMEs, i.e., bremsstrahlung, gyrosynchrotron emission and plasma emission. Among these emission types, bremsstrahlung emission is the main emission mechanism of the high-density plasma clouds of interplanetary CMEs. Gyrosynchrotron emission is the continuous emission generated by high-energy electrons from CMEs, while plasma emission is the main mechanism of transient radio bursts from CMEs. In this paper, the gyrosynchrotron emission of interplanetary CMEs is focused on. Firstly, the mechanism of gyrosynchrotron emission is reviewed. Secondly, a review of the physical parameter models of background solar wind and interplanetary CMEs is presented. After these, the brightness temperature and polarization of gyrosynchrotron emission of interplanetary CMEs are calculated and analyzed. Finally, the detectability of gyrosynchrotron emission of interplanetary CMEs by radio meters is discussed briefly.   相似文献   
80.
随着微放电效应研究的不断深入,低能电子影响在微放电过程中越来越不可忽视。当前常用的微放电模型在处理低能电子问题上具有一定的局限性,为了精确模拟这一过程,在深入研究二次电子和背散射电子发射理论的基础上,分别针对材料表面条件不同引起的二次电子发射系数不确定性、低能电子的背散射系数以及电子入射角等问题进行了分析和讨论,并在此基础上建立了一个二次电子发射模型,最后通过数值计算讨论了模型的正确性和适用范围。这一模型同时考虑材料表面条件参数、低能电子的背散射系数以及入射角等因素影响,能够兼容较低能量电子的二次发射,提升微放电数值模拟的精确度和适用性,为微放电数值模拟的发展起到推进作用。  相似文献   
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