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461.
R. C. Wiens D. S. Burnett C. M. Hohenberg A. Meshik V. Heber A. Grimberg R. Wieler D. B. Reisenfeld 《Space Science Reviews》2007,130(1-4):161-171
The Genesis mission returned samples of solar wind to Earth in September 2004 for ground-based analyses of solar-wind composition,
particularly for isotope ratios. Substrates, consisting mostly of high-purity semiconductor materials, were exposed to the
solar wind at L1 from December 2001 to April 2004. In addition to a bulk sample of the solar wind, separate samples of coronal
hole (CH), interstream (IS), and coronal mass ejection material were obtained. Although many substrates were broken upon landing
due to the failure to deploy the parachute, a number of results have been obtained, and most of the primary science objectives
will likely be met. These objectives include He, Ne, Ar, Kr, and Xe isotope ratios in the bulk solar wind and in different
solar-wind regimes, and 15N/14N and 18O/17O/16O to high precision. The greatest successes to date have been with the noble gases. Light noble gases from bulk solar wind
and separate solar-wind regime samples have now been analyzed. Helium results show clear evidence of isotopic fractionation
between CH and IS samples, consistent with simplistic Coulomb drag theory predictions of fractionation between the photosphere
and different solar-wind regimes, though fractionation by wave heating is also a possible explanation. Neon results from closed
system stepped etching of bulk metallic glass have revealed the nature of isotopic fractionation as a function of depth, which
in lunar samples have for years deceptively suggested the presence of an additional, energetic component in solar wind trapped
in lunar grains and meteorites. Isotope ratios of the heavy noble gases, nitrogen, and oxygen are in the process of being
measured. 相似文献
462.
J. Wicht M. Mandea F. Takahashi U. R. Christensen M. Matsushima B. Langlais 《Space Science Reviews》2007,132(2-4):261-290
Mariner 10 measurements proved the existence of a large-scale internal magnetic field on Mercury. The observed field amplitude,
however, is too weak to be compatible with typical convective planetary dynamos. The Lorentz force based on an extrapolation
of Mariner 10 data to the dynamo region is 10−4 times smaller than the Coriolis force. This is at odds with the idea that planetary dynamos are thought to work in the so-called
magnetostrophic regime, where Coriolis force and Lorentz force should be of comparable magnitude. Recent convective dynamo
simulations reviewed here seem to resolve this caveat. We show that the available convective power indeed suffices to drive
a magnetostrophic dynamo even when the heat flow though Mercury’s core–mantle boundary is subadiabatic, as suggested by thermal
evolution models. Two possible causes are analyzed that could explain why the observations do not reflect a stronger internal
field. First, toroidal magnetic fields can be strong but are confined to the conductive core, and second, the observations
do not resolve potentially strong small-scale contributions. We review different dynamo simulations that promote either or
both effects by (1) strongly driving convection, (2) assuming a particularly small inner core, or (3) assuming a very large
inner core. These models still fall somewhat short of explaining the low amplitude of Mariner 10 observations, but the incorporation
of an additional effect helps to reach this goal: The subadiabatic heat flow through Mercury’s core–mantle boundary may cause
the outer part of the core to be stably stratified, which would largely exclude convective motions in this region. The magnetic
field, which is small scale, strong, and very time dependent in the lower convective part of the core, must diffuse through
the stagnant layer. Here, the electromagnetic skin effect filters out the more rapidly varying high-order contributions and
mainly leaves behind the weaker and slower varying dipole and quadrupole components (Christensen in Nature 444:1056–1058,
2006). Messenger and BepiColombo data will allow us to discriminate between the various models in terms of the magnetic fields
spatial structure, its degree of axisymmetry, and its secular variation. 相似文献
463.
为进行燃气涡轮冷却结构的设计,在考虑总的温度分布系数(OTDF)及不考虑OTDF两种情况下,采用一套设计方法,完成了燃气涡轮第一级动叶冷却结构的整体设计。通过设计表明:采用管网计算,并通过三维导热计算进行热分析,最后通过气热耦合计算能够快速地设计出较佳的冷却结构;不考虑OTDF设计时,第一腔流量为16.9g/s,第二腔流量为40.8g/s,最大无量纲温度0.700,采用双进口蛇形通道,换热效果较佳,且结构设计较为简单;考虑OTDF时,为达到设计要求,第一腔流量为18.2g/s,第二腔流量为25.4g/s,第三腔流量为5.3g/s,最大无量纲温度0.752。通过多方案设计,得出在无气膜情况下,采用三个冷气进口多回转通道能够达到较好的冷却效果。 相似文献
464.
465.
高超声速飞行器机体/推进一体化设计的启示 总被引:6,自引:2,他引:6
机体/推进一体化设计是吸气式高超声速飞行器的关键技术。飞行器的前体和后体既是主要的气动型面,又是发动机进气道的外压缩型面和尾喷管的膨胀型面,一体化设计直接影响飞行器的气动与发动机性能。本文阐述了吸气式高超声速飞行器的主要特点,梳理了飞行器的推阻匹配、升阻比特性、操稳匹配等主要气动设计问题。通过对国外典型高超声速飞行器机体/推进一体化设计技术的综合分析,总结了前体/进气道、后体/尾喷管、边界层强制转捩装置等关键部件的气动设计方法,获得了有意义的启示,可为后续吸气式高超声速技术研究提供重要参考。 相似文献
466.
467.
航天器贮箱变质量流固耦合系统的动力学响应 总被引:1,自引:0,他引:1
研究了航天器贮箱变质量流固耦合系统的动力学特性.根据虚拟质量法(VMM),结合边界元法和有限元法构建了系统的动力学模型,建模过程中着重考虑了质量变化对系统的动态影响.通过Newmark直接积分法计算出贮箱变质量系统的振动响应.结果表明:由于系统质量减少,引起了系统振动频率的增大,并产生一个附加负阻尼.系统的振动频率的范围可以通过系统质量的范围确定.变质量引起的附加负阻尼的大小与系统的质量变化率成正比.对于系统的横向振动,质量减少引起的附加负阻尼在整个过程对系统振动的影响比较稳定,对于系统的纵向振动,质量减少引起的附加负阻尼对系统振动的影响随时间的增加而增大. 相似文献
468.
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470.