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111.
112.
为了探究影响含裂纹铝合金薄板材料断裂韧度、剩余强度的几何因素以及韧性材料的断裂机理,对典型航空铝合金2524-T3薄板,采用不同宽度、不同初始裂纹长度的中心裂纹板试样进行试验,测定材料的K-R阻力曲线,确定平面应力断裂韧度Kc和表观断裂韧度Kapp.试验结果表明:对于薄板结构,K-R阻力曲线与板宽相关;试件宽度、初始裂纹长度对断裂韧度和表观断裂韧度的确定都有影响,且板宽度的影响较大.基于上述结论,推荐两种可同时反映韧性材料断裂中的净截面屈服效应和韧性撕裂过程的剩余强度预测方法. 相似文献
113.
文章研究了矩阵方程的中心对称解.利用矩阵对的广义奇异值分解给出了该方程有中心对称解的充分必要条件,以及解的通式,证明了最佳逼近问题存在唯一解,并给出了求最佳逼近解的算法和数值箅例. 相似文献
114.
通过对Linux2.4.20版内核路由模块代码的分析和研究,详尽地阐述了Linux路由机制的实现思想和技术特点,对于更好地使用Linux的路由功能和在Linux路由上进行二次开发都具有实际的指导意义。 相似文献
115.
A Class of TVD Type Combined Numerical Scheme for MHD Equations With a Survey About Numerical Methods in Solar Wind Simulations 总被引:3,自引:0,他引:3
It has been believed that three-dimensional, numerical, magnetohydrodynamic (MHD) modelling must play a crucial role in a
seamless forecasting system. This system refers to space weather originating on the sun; propagation of disturbances through
the solar wind and interplanetary magnetic field (IMF), and thence, transmission into the magnetosphere, ionosphere, and thermosphere.
This role comes as no surprise to numerical modelers that participate in the numerical modelling of atmospheric environments
as well as the meteorological conditions at Earth. Space scientists have paid great attention to operational numerical space
weather prediction models. To this purpose practical progress has been made in the past years. Here first is reviewed the
progress of the numerical methods in solar wind modelling. Then, based on our discussion, a new numerical scheme of total
variation diminishing (TVD) type for magnetohydrodynamic equations in spherical coordinates is proposed by taking into account
convergence, stability and resolution. This new MHD model is established by solving the fluid equations of MHD system with
a modified Lax-Friedrichs scheme and the magnetic induction equations with MacCormack II scheme for the purpose of developing
a combined scheme of quick convergence as well as of TVD property. To verify the validation of the scheme, the propagation
of one-dimensional MHD fast and slow shock problem is discussed with the numerical results conforming to the existing results
obtained by the piece-wise parabolic method (PPM). Finally, some conclusions are made.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
116.
根据投放任务要求设计缩比可重复使用空间飞行器(RLV)投放轨迹,并建立飞行动力学基本分析框架。其中包括对轨迹进行参数灵敏度分析和沿轨迹的操稳特性分析。灵敏度分析则包括飞行终端状态参数受模型变化、投放条件、操纵参数、风场等内外扰动影响的分析。稳定性分析包括静稳定性和失速/偏离判据以及模态特性分析;操纵性分析包括考虑平衡、增稳和机动性余量三方面的要求。以上工作为导航和控制设计奠定了重要基础。 相似文献
117.
DECENTRALIZEDOUTPUTFEEDBACKFAULT一TOLERANTCONTROLFORUNCERTAINLARGE一SCALESYSTEMSHuShousong;FanCunhai(DepartmentofAutomaticConuo... 相似文献
118.
在激光测角干涉仪中,由于角度棱镜安置的方位不同,将导致该仪器角度测量范围的变化。分析了角度棱镜的方向和位置对角度测量范围的影响,比较了不同方案的优劣,并给出了结论。 相似文献
119.
120.
Alberto Buzzoni Giuseppe Altavilla Siwei Fan Carolin Frueh Italo Foppiani Marco Micheli Jaime Nomen Noelia Sánchez-Ortiz 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(1):371-393
We report on extensive photometry and low-resolution () spectroscopy of the deep-space debris WT1190F, which impacted Earth offshore from Sri Lanka, on 2015 November 13. In spite of its likely artificial origin (as a relic of some past lunar mission), the case offered important points of discussion for its suggestive connection with the envisaged scenario for a (potentially far more dangerous) natural impactor, like an asteroid or a comet.Our observations indicate for WT1190F an absolute magnitude , with a flat dependence of reflectance on the phase angle, such as ?mag?deg?1. The detected short-timescale variability suggests that the body was likely spinning with a period twice the nominal figure of , as from the observed lightcurve. In the color domain, WT1190F closely resembled the Planck deep-space probe. This match, together with a depressed reflectance around 4000 and 8500 Å may be suggestive of a “grey” (aluminized) surface texture.The spinning pattern remained in place also along the object fiery entry in the atmosphere, a feature that may have partly shielded the body along its fireball phase perhaps leading a large fraction of its mass to survive intact, now lying underwater along a tight (?km) strip of sea, at a depth of 1500?m or less.Under the assumption of Lambertian scatter, an inferred size of ?cm is obtained for WT1190F. By accounting for non-gravitational dynamical perturbations, the Area-to-Mass ratio of the body was in the range ?m2?kg?1.Both these figures resulted compatible with the two prevailing candidates to WT1190F’s identity, namely the Athena II Trans-Lunar Injection Stage of the Lunar Prospector mission, and the ascent stage of the Apollo 10 lunar module, callsign “Snoopy”. Both candidates have been analyzed in some detail here through accurate 3D CAD design mockup modelling and BRDF reflectance rendering to derive the inherent photometric properties to be compared with the observations. 相似文献