TC11合金高温变形行为及其机理

采用Gleeble-1500热模拟机研究了TC11合金在800～1 050℃、应变速率0.005～5/s条件下的高温变形行为.根据动力学分析,确定了不同温度区间的热激活能和热变形方程.结合变形微观组织观察确定了TC11合金的高温变形机制.结果显示:TC11合金在(α β)两相区和β相区的热变形激活能分别为285.38和141.98 kJ/mol,表明不同温度区间的热变形机理不同;在两相区变形主要发生片状组织的球化,在β相区变形时低应变速率下(0.005～0.05/s)主要发生β相的动态再结晶,高应变速率下(0.05～5/s)主要发生动态回复.研究结果为确定该合金的最佳变形工艺参数提供了理论依据.     

Elemental Abundances in Coronal Structures

A great deal of evidence for elemental abundance variations among different structures in the solar corona has accumulated over the years. Many of the observations show changes in the relative abundances of high- and low-First Ionization Potential elements, but relatively few show the absolute elemental abundances. Recent observations from the SOHO satellite give absolute abundances in coronal streamers. Along the streamer edges, and at low heights in the streamer, they show roughly photospheric abundances for the low-FIP elements, and a factor of 3 depletion of high-FIP elements. In the streamer core at 1.5 R·, both high- and low-FIP elements are depleted by an additional factor of 3, which appears to result from gravitational settling. This revised version was published online in June 2006 with corrections to the Cover Date.     

激波风洞重模型气动力试验研究

在激波风洞上进行气动力试验时,风洞启动时巨大的冲击载荷使模型-天平受到充分的激励,从而形成惯性干扰力,并与真实气动力混杂在一起,甚至完全覆盖气动力,降低了试验精准度,使得试验模型的质量受到极大的限制.本文介绍了CARDC-dia.2米激波风洞进行大、重模型的压电天平气动力试验研究情况,包括天平设计、天平校准、惯性补偿和风洞试验等几个方面.研究结果表明:气动力试验模型质量可从过去的500g增加到8kg,模型长度可达1m.从而提高了激波风洞测力试验能力,能满足高超声速飞行器试验的需求.