New Insights on Geomagnetic Storms from Model Simulations Using Multi-Spacecraft Data

The forecast of the terrestrial ring current as a major contributor to the stormtime Dst index and a predictor of geomagnetic storms is of central interest to ‘space weather’ programs. We thus discuss the dynamical coupling of the solar wind to the Earth's magnetosphere during several geomagnetic storms using our ring current-atmosphere interactions model and coordinated space-borne data sets. Our model calculates the temporal and spatial evolution of H⁺, O⁺, and He⁺ ion distribution functions considering time-dependent inflow from the magnetotail, adiabatic drifts, and outflow from the dayside magnetopause. Losses due to charge exchange, Coulomb collisions, and scattering by EMIC waves are included as well. As initial and boundary conditions we use complementary data sets from spacecraft located at key regions in the inner magnetosphere, Polar and the geosynchronous LANL satellites. We present recent model simulations of the stormtime ring current energization due to the enhanced large-scale convection electric field, which show the transition from an asymmetric to a symmetric ring current during the storm and challenge the standard theories of (a) substorm-driven, and (b) symmetric ring current. Near minimum Dst there is a factor of ∼ 10 variation in the intensity of the dominant ring current ion specie with magnetic local time, its energy density reaching maximum in the premidnight to postmidnight region. We find that the O⁺ content of the ring current increases after interplanetary shocks and reaches largest values near Dst minimum; ∼ 60% of the total ring current energy was carried by O⁺ during the main phase of the 15 July 2000 storm. The effects of magnetospheric convection and losses due to collisions and wave-particle interactions on the global ring current energy balance are calculated during different storm phases and intercompared. This revised version was published online in August 2006 with corrections to the Cover Date.     

直升机低速飞行特性与意外右偏航

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带伺服滑环和空气静压轴承的转台主轴干扰力矩的实验研究

带滑环伺服系统且采用空气静压气浮轴承的高精度陀螺漂移伺服转台，其控制精度受到气浮轴承粘滞力矩、涡流力矩、轴系质量配置不当造成的静不平衡力矩和滑环伺服系统对主轴干扰力矩的影响。本文通过理论分析和实验研究认为，当主轴轴系垂直于地面放置时，其主要干扰力矩来自滑环伺服系统。论文在对实验数据进行各项检验和处理的基础上给出了主轴常值和随机干扰力矩的数学表达式，为进一步提高同类伺服转台的伺服精度提供了一条有效的途径。     

O型橡胶密封圈截径测量方法的研究

O型橡胶密封圈截径的测量并没有成型的结论。本文介绍了两种常见测量方法,并通过测量数据和气密性试验的对比阐述两种方法的优缺点。     

法兰连接密封结构的贮存可靠性分析

确定了固体火箭发动机法兰连接密封结构的失效模式，并用多模式结构可靠性分析方法对法兰连接密封结构的可靠性进行了分析和评估，给出了对接密封结构的可靠性随时间的规律，以及长期贮存的可靠寿命。     

有1的结合环的交换性

本文证明了有１的结合环的两个交换性定理，推广了Ｇｉｒｉ．Ｒ．Ｄ等人在参考文献１中的结果。     

一类具有饱和功能性反应的食饵-捕食者系统的定性分析

研究了具有饱和功能性反应的食饵—捕食者两种群模型:dxdt=xg(x)-yφ(x),dydt=y[-d eφ(x)]。分析了该系统的平衡点的类型,及平衡点稳定性。运用Du lac函数法,得到了系统不存在极限环的充分条件。运用Pioncare-Bendixson环域定理,证明了该系统存在极限环的充分条件。     

一种铁磁流体密封系统的理论研究

利用磁路方法和简化的Ｎａｖｉｅｒ－Ｓｔｏｋｅｓ方程，导出了锥形空间内磁场强度分布和旋转时铁磁流体稳定界面的计算方程。分析了密封间隙、密封角和转速对密封能力的影响。     

带箍环掠型叶片整体叶盘强度分析方法研究

针对带复合材料箍环掠型叶片整体叶盘结构，开发了对叶片快速施加气动载荷的方法，发现了整体叶盘的应力应变分析和寿命预测方法，成功地完成了模型叶盘的应变测量和低循环疲劳试验。通过模型叶盘数值分析与试验测量数据的比较可见，二吻合较好，从而验证了上述方法的有效性。     

往复轴密封间隙内磁性液体流动状态的研究

为了解决往复轴磁性液体密封中存在的问题,研究了往复轴以不同速度和行程运动时,密封间隙内磁性液体的流动状态,重点研究了往复轴密封间隙内磁性液体流动机理、往复轴运动所带走磁性液体的量、往复轴磁性液体密封的失效原因及往复轴磁性液体密封新结构的设计.实践表明所设计的新结构在某些应用场合是非常有效的.