用最优轨迹分析法研究战斗机的敏捷性

利用最优轨迹分析法确定战斗机的敏捷性，并将最优控制问题转换为参数优化问题，由非线性数学规划理论解出参数变化规律。从典型示例飞机分析了不同迎角限制和推力下的控制策略及对功能敏捷性的影响。仿真结果表明，在转弯过程中适当放宽迎角限制和增加推力都能增大转弯速率，缩短转弯时间，从而改善飞机的功能敏捷性。     

电传操纵系统设计中遇到的突出问题和对策

本文通过简要的理论分析及试验研究对电传纵向控制律设计中出现的一些实际问题,例如反馈形式、混合比、主增益、校正环节和滤波器等的选择;排除剩余振荡;对飞行品质的影响等做了较为充分有益的探讨.这对电传系统设计和改善飞行品质有参考作用.     

热力学模型在氮氧化物陶瓷研究中的应用

用热力学几何规则，对Si3N4-AlN-Al2O3-SiO2体系中的部分化舍物的标准生成吉布斯自由能进行了预报和评估；用新几何模型计算了Al2O3-SiO2-Si3N4三元体系高温液相的热力学性质。为研究Si3N4-AlN-Al2O3-SiO2体系陶瓷材料在制备和应用条件下的物理化学变化规律提供了热力学数据。此外，根据预报的热力学数据，计算并给出了Al-O-N、Si-O-N和B-O-N体系的参数状态图，为分析和确定O-Sialon-BN系复合材料合成和应用的条件提供了理论依据。     

富氧预燃室初步试验研究

为了研究全流量补燃循环发动机中富氧预燃室的点火以及燃烧特性，对点火方案和预燃室方案进行了分析。通过对多种预燃室结构形式和点火方式的比较，提出了适合于富氧预燃室初步试验要求的点火方案，研制了热表面谐振点火器并采用间接点火方式研制了氢氧火炬点火器。点火器的试验结果表明氢氧火炬点火器能够多次可靠地点火并生成稳定的点火火炬。由于不受谐振产生条件的限制，氢气和氧气的流量和混合比可以在较大的范围内选择，生成点火火炬的温度范围也很宽。对确定的富氧预燃室方案进行了设计加工，经过三个阶段的热试车，富氧预燃室的关键参数均达到了设计要求，结构无烧蚀，工作可靠，完全可以满足全流量补燃循环发动机系统对富氧预燃室的要求。     

火箭基组合循环(RBCC)推进系统研究现状

对火箭基组合循环(RBCC)推进系统基本概念进行了介绍，并就此项技术在美国的研究现状做了比较详细的综述，指出了发展这种新型推进装置的关键技术，对国内在这方面的研究思路提出了建议。     

Modeling and analysis of floating performances of stratospheric semi-rigid airships

In recent years, the study of semi-rigid airship has revived with the development of airships. Semi-rigid airships have some characteristics of rigid airships and non-rigid airships. Due to the flexibility of the envelope of the non-rigid airship, the variation of the temperature of the inner gas will lead to its structure deformation and affect its flight altitude. This paper develops the structural mechanics model, thermodynamic model and dynamic model of the semi-rigid airship, based on which nonlinear finite element analysis is employed for geometrically nonlinear deformation of the airship upper film in consideration of thermodynamics and structural mechanics coupling. Based on the thermal-structural interaction, the thermal characteristics and flight performances of the airship during floating flight are investigated. The 3-D solar radiation and temperature distribution of the airship skin and the temperature variation of the inner gas are presented to investigate the thermal performance of the airship, flight velocity, acceleration and flight altitude are simulated to investigate the flight performance, and the variations of the volume and pressure difference of the inner gas are calculated to provide a basis for structure design. The results of the simulation can be referenced for the design of the semi-rigid airship, and can be used for the further study on the attitude control of the airship during its floating flight.     

Simulated microgravity inhibits the proliferation of K562 erythroleukemia cells but does not result in apoptosis

Astronauts and experimental animals in space develop the anemia of space flight, but the underlying mechanisms are still unclear. In this study, the impact of simulated microgravity on proliferation, cell death, cell cycle progress and cytoskeleton of erythroid progenitor-like K562 leukemia cells was observed. K562 cells were cultured in NASA Rotary Cell Culture System (RCCS) that was used to simulate microgravity (at 15 rpm). After culture for 24 h, 48 h, 72 h, and 96 h, the cell densities cultured in RCCS were only 55.5%, 54.3%, 67.2% and 66.4% of the flask-cultured control cells, respectively. The percentages of trypan blue-stained dead cells and the percentages of apoptotic cells demonstrated no difference between RCCS-cultured cells and flask-cultured cells at every time points (from 12 h to 96 h). Compared with flask-cultured cells, RCCS culture induced an accumulation of cell number at S phase concomitant with a decrease at G0/G1 and G2/M phases at 12 h. But 12 h later (from 24 h to 60 h), the distribution of cell cycle phases in RCCS-cultured cells became no difference compared to flask-cultured cells. Consistent with the changes of cell cycle distribution, the levels of intercellular cyclins in RCCS-cultured cells changed at 12 h, including a decrease in cyclin A, and the increasing in cyclin B, D1 and E, and then (from 24 h to 36 h) began to restore to control levels. After RCCS culture for 12–36 h, the microfilaments showed uneven and clustered distribution, and the microtubules were highly disorganized. These results indicated that RCCS-simulated microgravity could induce a transient inhibition of proliferation, but not result in apoptosis, which could involve in the development of space flight anemia. K562 cells could be a useful model to research the effects of microgravity on differentiation and proliferation of hematopoietic cells.     

导引系统环境应力筛选设计

依据环境应力筛选的基本特征,结合某型炸弹导引系统的结构特点,制定了产品的初始环境应力筛选方案.通过产品的设计定型试验,验证了最终的环境应力筛选方案是行之有效的.     

CFRP超高周疲劳损伤演化过程

碳纤维增强树脂基复合材料（CFRP）在航空航天等领域得到广泛应用，CFRP构件的超高周疲劳问题逐渐凸显出来。本文采用超声三点弯曲疲劳试验系统对CFRP复合材料的损伤演化过程进行研究。结果表明：CFRP复合材料在超高周三点弯曲加载下的S-N曲线呈阶梯状，尤其在10⁸周次后，其疲劳强度明显下降。通过对CFRP复合材料在同一视场不同周次下的损伤过程进行分析，发现该材料在超高周加载下的损伤形貌主要表现为3种特征：纤维束交叉处基体损坏、近纤维束平行段基体空洞、基体贯穿，并随着加载周次的增加，其损伤过程也按照这3种特征依次呈现出来。