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11.
A numerical procedure for the calculation of the transonic dip of airfoils in the time domain is presented. A viscous-inviscid aerodynamic interaction method is taken to calculate the unsteady aerodynamic loads. In the present case the integral boundary layer equations are coupled with the Transonic Small Disturbance (TSD) Potential Equation. The coupling between structural motion and aerodynamic loads is carried out using State Space equation. It is solved by State Transition Matrix technique. Results are presented for NACA 64A010 and NLR 7301 airfoils with structural data from Isogai and DLR, respectively. Comparisons show good agreement with other numerical results. Certain deviations of experimental data taken from literature need more insight in the detailed test conditions. 相似文献
12.
Kamide Y. Kihn E.A. Ridley A.J. Cliver E.W. Kadowaki Y. 《Space Science Reviews》2003,107(1-2):307-316
We report the recent progress in our joint program of real-time mapping of ionospheric electric fields and currents and field-aligned
currents through the Geospace Environment Data Analysis System (GEDAS) at the Solar-Terrestrial Environment Laboratory and
similar computer systems in the world. Data from individual ground magnetometers as well as from the solar wind are collected
by these systems and are used as input for the KRM and AMIE magnetogram-inversion algorithms, which calculate the two-dimensional
distribution of the ionospheric parameters. One of the goals of this program is to specify the solar-terrestrial environment
in terms of ionospheric processes, providing the scientific community with more than what geomagnetic activity indices and
statistical models provide.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
13.
阐述了研制全天球实时恒星模拟器的意义以及国内外发展趋势,介绍第二代恒星模拟器的系统组成、特点、技术指标以及解决的技术问题。 相似文献
14.
Steven D. Howe 《Space Policy》2001,17(4):275-283
The potential benefits to humankind of space exploration are tremendous. Space is not only the final frontier but is also the next marketplace. The orbital space above Earth offers tremendous opportunities for both strategic assets and commercial development. The critical obstacle retarding the use of the space around the Earth is the lack of low cost access to orbit. Further out, the next giant leap for mankind will be the human exploration of Mars. Almost certainly within the next 30 years, a human crew will brave the isolation, the radiation, and the lack of gravity to walk on and explore the Red planet. Both of these missions will change the outlook and perspective of every human being on the planet. However, these missions are expensive and extremely difficult. Chemical propulsion has demonstrated an inability to achieve orbit cheaply and is a very high-risk option to accomplish the Mars mission. An alternative solution is to develop a high performance propulsion system. Nuclear propulsion has the potential to be such a system. The question will be whether humanity is willing to take on the challenge. 相似文献
15.
雷呈凤 《南昌航空工业学院学报》2004,18(1):24-27
通过构造基本群的正规子群,得到有限复迭空间和自映射的提升。并定义了NL数,指出用NL数可以估算自映射的Nielsen数。 相似文献
16.
Terrestrial technology is now, and increasingly, sensitive to space weather. Most space weather is caused by solar storms
and the resulting changes to the Earth's radiation environment and the magnetosphere. The Sun as the driver of space weather
is under intense observation but remains to be adequately modelled. Recent spacecraft measurements are greatly improving models
of solar activity, the interaction of the solar wind with the magnetosphere, and models of the radiation belts. In-situ data
updates the basic magnetospheric model to provide specific details of high-energy electron flux at satellite orbits. Shock
wave effects at the magnetopause can also be coarsely predicted. However, the specific geomagnetic effects at ground level
depend on the calculation of magnetic and electric fields and further improvements are needed. New work on physical models
is showing promise of raising geomagnetic and ionospheric predictability above the synoptic climatological level.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
17.
18.
介绍了卫星在热平衡试验后所发现的有效载荷的污染情况,通过对污染提取物的分析和试验设备的再次污染监测,找出了污染源,并对以后的防污染工作提供了借鉴. 相似文献
19.
介绍了大型空间模拟器真空测量自动化的实施和特点,以及真空度的描述方法,对真空测量自动化的进一步发展提出了设想。 相似文献
20.
Spall caused by hypervelocity impacts at the lower range of velocities could result in significant damage to spacecraft. A number of polycrystalline alloys, used in spacecraft manufacturing, exhibit a pronounced anisotropy in their mechanical properties. The aluminium alloy AA 7010, whose orthotropy is a consequence of the meso-scale phase distribution or grain morphology, has been chosen for this investigation. The material failure observed in plate impact was simulated using a number of spall models. The Hugoniot elastic limit and spall strength have been studied as a function of orientation, and compared to experimental results. 相似文献