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C. Wang J.D. Richardson 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2005,35(12):2102-2105
We review recent Voyager 2 observations in the vicinity of 70 AU. The character of the solar wind plasma data between 2002 and 2003 changed to a regime in which the speed, density and magnetic field magnitude are positively correlated. The average speed of the solar wind at Voyager 2 increased between early 2003 and mid-2004, which we attribute to a return of fast coronal hole flow. We use solar wind data at Earth as input to numerical models which include the effect of pickup ions to model the radial evolution of the solar wind. The model reproduces the basic features of the observations. As a specific example, we investigate the propagation of the Halloween (Oct.–Nov.), 2003 storms in the outer heliosphere. The model predictions are in reasonable agreement with Voyager 2 observations. 相似文献
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将实际的太阳大气划分为多个等温层次,导出了均匀倾斜磁场下线性Alfven波通过任意多等温层的能量透射率,结果表明,两等温层模式与三等温层模式的结果存在本质的区别。在两等温层中,温度的跃变式增高对Alfven波起着高通滤波的作用,而三等温层中在高频端Alfven波的透射率显示为振荡形态,对实际大气温度模式的计算结果表明,太阳低层大气更适合于周期为数秒的Alfven波的能量传输。 相似文献
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M. Verigin D. Vignes D. Crider J. Slavin M. Acua G. Kotova A. Remizov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,33(12):2222-2227
The origin of the anisotropy in the shape of the Martian obstacle and bow shock is analyzed using Mars Global Surveyor observations. The influence of MHD or ion pick-up effects on Martian obstacle position was to be small found, however, localized Martian crustal magnetization increases the thickness of the downstream planetary magnetotail by 500–1000 km in agreement with earlier Phobos 2 observations. A new analytical model is presented for Martian obstacle shape variation for different solar wind ram pressure. Elongation of the Martian BS cross-section in the direction perpendicular to IMF was confirmed while the shift of this cross section in the +Y direction of Martian interplanetary medium reference frame was discovered. The shift of BS cross section in the direction of interplanetary electric field was not revealed thus not conforming the idea that mass-loading play some role in BS control. 相似文献
917.
高灵敏度莫尔偏折法及其在激波风洞流场中的应用 总被引:2,自引:0,他引:2
本文介绍了一种具有高灵敏度的莫尔偏折法,从理论上分析了其工作和测量原理。并把这种方法用于高超声速激波风洞中流场的显示和测量,获得了几种特殊模型流场的清晰莫尔偏折图,定量计算了高超声速激波风洞中带有凸起物模型三维密度场的分布。 相似文献
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Impulsively starting flow, by a sudden attainment of a large angle of attack, has been well studied for incompressible and supersonic flows, but less studied for subsonic flow. Recently, a preliminary numerical study for subsonic starting flow at a high angle of attack displays an advance of stall around a Mach number of 0.5, when compared to other Mach numbers. To see what happens in this special case, we conduct here in this paper a further study for this case, to display and analyze the full flow structures. We find that for a Mach number around 0.5, a local supersonic flow region repeatedly splits and merges, and a pair of left-going and right-going unsteady shock waves are embedded inside the leading edge vortex once it is sufficiently grown up and detached from the leading edge. The flow evolution during the formation of shock waves is displayed in detail. The reason for the formation of these shock waves is explained here using the Laval nozzle flow theory. The existence of this shock pair inside the vortex, for a Mach number only close to 0.5, may help the growing of the trailing edge vortex responsible for the advance of stall observed previously. 相似文献