机载三股流板翅式冷凝器数值计算与实验研究

分析了翅片、隔板和流体的传热规律,采用有限容积法建立了包含相变流和交叉式在内的多股流板翅式换热器数学模型。基于蒸发制冷循环试验台,在4种工况条件下对机载交叉式三股流板翅式冷凝器换热性能进行了实验,并在特定工况下,通过温度场分析了各股流体间的换热特性。经数值计算与实验结果的对比,流体换热量的最大相对误差为8.08%,满足工程设计计算需求。通过定性分析,认为流体流量分配不均、相变流体潜热以及相变对流表面换热系数的计算是误差的主要来源。     

基于MPP编程环境的一种并行子空间迭代法

子空间迭代法是科学与工程计算中求解广义特征值问题的有效方法 ,针对向量机和共享内存的多处理机 ,前人已成功地作了并行处理。文中给出了适合 MPP大规模并行计算机的并行子空间迭代法。该算法将广义特征值问题转换为一般特征值问题 ,其计算工作量主要体现在矩阵乘法 ,通过对该方法作并行处理 ,使矩阵求逆及一部分乘法运算转换为各结点机上三角形方程组的并行求解。在大规模并行计算机 PA R95上结合 J8- II机翼的动力特性问题对该算法作了数值试验 ,结果说明所给算法是非常有效的     

The hydroxyl radical as an indicator of SEP fluxes in the high-latitude terrestrial atmosphere

The low background values at nighttime of the mesospheric hydroxyl (OH) radical make it easier to single out the atmospheric response to the external solar forcing in Polar Regions. Because of the short lifetime of HO_x, it is possible to follow the trails of Solar Energetic Particle (SEP) events in the terrestrial atmosphere, as shown by Storini and Damiani (2008). The sensitivity of this indicator makes discernible not only extreme particle events with a flux peak of several thousand pfu [1 pfu = 1 particle/(cm² s sr)] at energies >10 MeV, but also those with lower flux up to about 300 pfu. Using data from the Microwave Limb Sounder (MLS) on board the EOS AURA satellite, we examined the correlation of OH abundance vs. solar proton flux for almost all the identified SEP events spanning from November 2004 to December 2006 (later on no more SEP events occurred during Solar Cycle no. 23). The channels at energies greater than 5 MeV and 10 MeV showed the best correlation values (r ∼ 0.90–0.95) at altitudes around 65–75 km whereas, as expected, the most energetic channels were most highly correlated at lower altitudes. Therefore, it is reasonably possible to estimate the solar proton flux from values of mesospheric OH (and viceversa) and it could be useful in studying periods with gaps in the records of solar particles.     

基于剪裁技术考虑的某冲击试验分析

利用环境工程剪裁技术对某冲击试验的结果进行分析,结果表明,按照引用标准评定为"超差"的试验,当考虑到试验件结构的特性并进行必要的数据转换后,试验结果是有效。首先分析造成超差的原因为天线组件的剩余响应,然后通过频域数字滤波进行数据转换。     

Integrity of sulfur concrete subjected to simulated lunar temperature cycles

In view of potential application as a construction material on the lunar surface the mechanical integrity of sulfur concrete was evaluated after being subjected to simulated temperature cycles. Here, small cubes of sulfur concrete were repeatedly cycled between room (20 °C) and liquid nitrogen (−191 °C) temperatures after which they, and non-cycled cubes, were evaluated by compression testing. The compression strength of the non-cycled samples averaged ∼35 MPa (5076 psi) before failing whereas the cycled samples fractured at about 7 MPa (1015 psi). Microscopic examination of the fracture surfaces from the cycled samples showed clear de-bonding of the sulfur from the aggregate whereas it was seen adhering in those non-cycled. Based on a simple analysis it was concluded that the large strength discrepancy between cycled and non-cycled samples is due to differences between the coefficients of thermal expansion of the materials constituting the concrete.     

装备复杂电磁环境适应性试验问题探讨

从环境适应性概念入手,提出装备复杂电磁环境适应能力总体需求及适应性试验的基本构成,指出装备复杂电磁环境适应性试验应该具体涵盖雷电类、静电类、电磁兼容类、电子对抗类、强电磁脉冲类等五类试验内容。同时阐述了国内外在适应性试验研究方面的发展现状和遇到的挑战,为后续研究提供重要参考。     

先进的宇航试验舱温控系统

介绍了中国新一代宇航试验舱的温控系统。该温控系统设计思想先进、结构新颖。在直径２．３ｍ，长２ｍ的封闭舱体控温面上，实现了０℃～５０℃的任意温度定点控制及９０ｍｉｎ内的正弦波、梯形波、三角波的周期变化；在整个控温面上温度非均匀性（均方根偏差）小于０．３℃，远远超过了非均匀度±１℃、控制精度±２℃的原设计指标。     

月面探测器月夜休眠自主唤醒方法

提出一种月面探测器休眠自主唤醒方法:月夜来临时通过地面控制对月面探测器所有设备进行休眠操作;月昼来临时靠太阳光触发唤醒功能,由休眠唤醒电路自主发送指令唤醒探测器,解决月面探测器安全可靠度过月夜的能源供给问题。该方法已通过在轨验证,可为其他深空探测任务提供参考。     

无线传感器网络定位算法改进

提出了一种建立在TEEN协议基础之上反应式网络的应用.反应式网络是一种对适时性要求较高的网络,用三角定位法对传感器节点进行定位,在定位的基础上,使得簇首节点的选定更为容易,在一定程度上能节省节点能源、延长网络寿命.