喷管进口和喉道几何形状对固体火箭发动机比冲的影响

本文介绍在火箭喷管进口和喉道区域计算完全耦合的燃气——粒子混合物流场的计算机化模型。定常态的燃气流场是作为长时间渐近解计算的,而粒子流场是假定准定常流来计算。对于超音速燃气粒子流场,这一模型则与特征线法结合进行计算。计算表明喷管进口角度、喷管喉道曲率半径比、喉道尺寸以及粒子大小对比冲的影响。文中也介绍了一些发动机试验数据的比较。     

Hydrothermal simulation experiments as a tool for studies of the origin of life on Earth and other terrestrial planets: a review

The potential of life's origin in submarine hydrothermal systems has been evaluated by a number of investigators by conducting high temperature-high pressure experiments involving organic compounds. In the majority of these experiments little attention has been paid to the importance of constraining important parameters, such as the pH and the redox state of the system. This is particularly revealed in the apparent difficulties in interpreting experimental data from hydrothermal organic synthesis and stability studies. However, in those cases where common mineral assemblages have been used in an attempt to buffer the pH and redox conditions to geologically and geochemically realistic values, theoretical and experimental data seem to converge. The use of mineral buffer assemblages provides a convenient way by which to constrain the experimental conditions. Studies at high temperatures and pressure in the laboratory have revealed a number of reactions that proceed rapidly in hydrothermal fluids, including the Strecker synthesis of amino acids. In other cases, the verification of postulated abiotic reaction mechanisms has not been possible, at least for large molecules such as large fatty acids and hydrocarbons. This includes the Fischer-Tropsch synthesis reaction. High temperature-high pressure experimental methods have been developed and used successfully for a long time in, for example, mineral solubility studies under hydrothermal conditions. By taking advantage of this experimental experience new and, at times, unexpected directions can be taken in bioorganic geochemistry, one being, for instance, primitive two-dimensional information coding. This article critically reviews some of the organic synthesis and stability experiments that have been conducted under simulated submarine hydrothermal conditions. We also discuss some of the theoretical and practical considerations that apply to hydrothermal laboratory studies of organic molecules related to the origin of life on Earth and probably also to the other terrestrial planets.     

海湾战争与美国E—3预警机

海湾战争中,美国E-3预警机战功显赫。本文详述E-3预警机研制过程,基本规格,目前生产型号,航空电子装备,以及未来的技术改造。     

疾风劲草,板荡诚臣——为张处弘鼓与呼

唐李世民《赐萧瑀》一诗中说:“疾风知劲草,板荡识诚臣。勇夫安识义?智者必怀仁。”前两句是说在严峻时势的考验下,才能识别忠良。“板荡”系指《诗·大雅》中的《板》、《荡》两诗,反映周厉王时期动荡、艰难的社会情况,后遂以“板荡”比喻艰难动荡之世。张处弘——中国航空史研究会副理事长,浙江航空学会前理事长、杭州蓝天飞艇技术研究所所长,是疾风中的“劲草”,艰辛中的“诚臣”,不是李世民诗句中所说的徒有一时之勇的勇夫,而是中国航空战线上的真正勇士,航空科技事业的智者！张处弘同志在空军工作多年,离开部队时本可以以相当高的级别安享晚年,但他却一心扑向了研制飞艇的事业,靠自己的力量办起了民办航空研究所,并完全凭自己的努力,历尽千难万苦,中国人自己研制的载人飞艇获得成功。正当张处弘的飞艇事业向更大的成     

FL—1风洞攻角控制系统设计

本文介绍了ＦＬ－１风洞攻角（飞机模型的俯卸角）控制系统的理件和软件配置，介绍了ＰＣ机在工业控制系统中的应用。叙述了把十四位并行二进制码实时转换成攻角（度）的方法，以及在ＰＣ机上用高级语言编写的主程序调用汇编语言编写的子程序的方法。     

返回式卫星数字姿态控制系统及飞行试验结果

简要介绍我国返回式卫星上用的计算机数字姿态控制系统的方案;重点阐述姿态确定和相平面控制律的设计方法;最后简述飞行试验的结果。     

评定运载火箭成本的TRANSCOST模型及其应用

首先介绍评定运载火箭的研制和发射成本的解析模型的结构,着重讨论评定使用成本的新方法,并引入众多参数来修正模型.尔后以“阿里安”4后继型为例,讨论用于未来系统分析和成本比较的模型,分析了采用10种不同方案的可贮低温燃料两级火箭的研制和发射成本.欧洲未来运载火箭系统的关键是要最佳解决有限的研制费用与期望的最低发射成本之间的矛盾.多次使用系统能使发射成本大为降低,但研制费用较大.基于实际参数的成本解析模型能为选择运载火箭方案提供重要的信息.     

径向磁气组合轴承系统的动态性能

为探究磁轴承失效时能否减轻转子跌落带来的损害,将人字槽径向动压气体轴承引入磁轴承转子系统,研究磁气组合轴承对系统动态性能的影响和动压气体轴承的支承特性。采用有限差分法和小扰动法求解气膜厚度方程和雷诺方程,研究动压气体轴承的静动态特性。对磁轴承电磁力进行了分析,采用磁轴承不完全微分PID（比例-积分-微分）控制策略,对系统进行了理论模态分析和试验模态分析,完成了系统高速旋转试验,测试了动压气体轴承在不同偏心率和转速下的承载力。结果表明,引入动压气体轴承可提高系统的动态性能,在磁轴承失效造成高速转子跌落瞬间,偏心率趋近于1,两个径向动压气体轴承能够产生较大承载力,减轻转子跌落造成的损害。      

基于AMESim的隔舱式贮箱推进剂管理仿真研究

通过多学科动力学建模方法研究,利用AMESim建立了隔舱式贮箱推进剂输送系统机械、液流与控制动力学模型,并对不同工况下推进剂输送系统动态特性进行数值仿真,获得了隔舱式贮箱推进剂动态变化、各个隔舱 的推进剂消耗率及质心位移等结果.仿真结果显示隔舱总体布局与初始容积分配、隔舱连通结构、飞行轨迹等均对隔舱式贮箱推进剂动态变化产生影响,所建立的模型可应用于隔舱式贮箱总体及结构设计.