某型飞机水平加速性能试飞换算结果及误差分析

从最基本的质心运动方程出发，通过飞机运动基本假设，运用相似原理和微分修正量法，推导出飞机水平加速性能向定高度换算的公式。结合某型飞机的试飞给出换算结果实例，并与以前换算方法得到的结果进行比较，说明此换算方法原理正确，可以为飞机性能研究人员提供参考。     

Applied superconductivity and superfluidity for the exploration of the Moon and Mars.

We discuss how superconductivity and superfluidity can be applied to solve the challenges in the exploration of the Moon and Mars. High sensitivity instruments using phenomena of superconductivity and superfluidity can potentially make significant contributions to the fields of navigation, automation, habitation, and resource location. Using the quantum nature of superconductivity, lightweight and very sensitive diagnostic tools can be made to monitor the health of astronauts. Moreover, the Moon and Mars offer a unique environment for scientific exploration. We also discuss how powerful superconducting instruments may enable scientists to seek answers to several profound questions about nature. These answers will not only deepen our appreciation of the universe, they may also open the door to paradigm-shifting technologies.     

Reliability Analysis of Aircraft Condition Monitoring Network Using an Enhanced BDD Algorithm

The aircraft condition monitoring network is responsible for collecting the status of each component in aircraft. The reliability of this network has a significant effect on safety of the aircraft. The aircraft condition monitoring network works in a real-time manner that all the data should be transmitted within the deadline to ensure that the control center makes proper decision in time. Only the connectedness between the source node and destination cannot guarantee the data to be transmitted in time. In this paper, we take the time deadline into account and build the task-based reliability model. The binary decision diagram (BDD), which has the merit of efficiency in computing and storage space, is introduced when calculating the reliability of the network and addressing the essential variable. A case is analyzed using the algorithm proposed in this paper. The experimental results show that our method is efficient and proper for the reliability analysis of the real-time network.     

交流变频调速系统的SPWM波形生成方法的谐波分析

本文简述了交流变频调速系统常用的四种ＳＰＷＭ波形生成的方法，并研究了各种方法的ＳＰＷＭ开关点计算公式及其推导，利用这些公式计算了一系列开关点数据，同时提出了一种以开关点数据分析ＳＰＷＭ波形各次谐波的方法，通过谐波分析证实自然采样法优于其他方法。     

应用S-A模型的自由射流和冲击射流数值模拟

为探索轴对称射流准确的数值模拟方法，根据可压缩的轴对称N-S方程，利用二阶精度的有限体积法对轴对称的自由射流和垂直冲击射流进行数值模拟。结果表明采用Spalart-Allmaras湍流模型，可很好描述射流流动。收缩喷嘴射流计算应从出口上游的内流开始，而不能在出口截面上给定声速条件。计算结果与实验吻合较好，所获得的喷嘴内外部流场的流动状况以及冲击射流参数分布，可用于优化喷嘴内部结构设计。     

高超声速乘波飞行器气动实验研究

以绕楔高超声速流场为基础，用流线追踪法生成了一种高超声速飞行器气动概念构形、初步探索了高超声速飞行器机身/推进系统一体化气动构形设计方法，开展了高超声速测压实验，结果表明：该类构形飞行器在高超声速飞行时，可以产生较高的升阻比，前体的预压缩效果明显，是以吸气式冲压发动机动力的有效途的飞行器构形。     

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Multi-objective evolutionary design of selective triple modular redundancy systems against SEUs

To improve the reliability of spaceborne electronic systems,a fault-tolerant strategy of selective triple modular redundancy(STMR)based on multi-objective optimization and evolvable hardware(EHW)against single-event upsets(SEUs)for circuits implemented on field programmable gate arrays(FPGAs)based on static random access memory(SRAM)is presented in this paper.Various topologies of circuit with the same functionality are evolved using EHW firstly.Then the SEU-sensitive gates of each circuit are identified using signal probabilities of all the lines in it,and each circuit is hardened against SEUs by selectively applying triple modular redundancy(TMR)to these SEU-sensitive gates.Afterward,each circuit hardened has been evaluated by SEU Simulation,and the multi-objective optimization technology is introduced to optimize the area overhead and the number of functional errors of all the circuits.The proposed fault-tolerant strategy is tested on four circuits from microelectronics center of North Carolina(MCNC)benchmark suite.The experimental results show that it can generate innovative trade-off solutions to compromise between hardware resource consumption and system reliability.The maximum savings in the area overhead of the STMR circuit over the full TMR design is 58%with the same SEU immunity.     

铝合金等离子体微弧氧化陶瓷层组织与性能研究

采用扫描电子显微镜(SEM)、X射线衍射(XRD)分析了LY12铝合金表面陶瓷层的形貌和相组成,用纳米显微力学探针测定了陶瓷层的纳米硬度和弹性模量。结果表明,陶瓷层具有表面疏松层和内部致密层两层结构,陶瓷层主要由α Al2O3和γ Al2O3组成,纳米硬度和弹性模量在陶瓷层截面的分布情况相似,由内层到外层呈降低趋势。     

喷丸产生的残余拉应力场及材料的内部疲劳极限

 本文采用大型弹塑性分析有限元程序ADINA-84计算了40Cr钢9种规范的喷丸残余应力场,获得了残余拉应力场的计算表达式,并根据疲劳试验结果,提出了内部疲劳极限概念及喷丸强化的内部疲劳极限理论。