直升机着舰起落架动态响应

舰载直升机着舰过程复杂。与地面降落相比,舰面的不稳定气流使得直升机姿态难以保持,下降的速度更大,且由于直升机通常都是单轮着舰,导致起落架载荷很大。为了研究直升机在不同条件下着舰时起落架的动态响应,建立了机体/起落架/舰船耦合模型,将着舰过程中直升机的运动和舰船的运动联系起来,通过仿真计算得出起落架的动态响应。仿真计算结果表明:直升机着舰质量越大,起落架压缩量和载荷越大;直升机低头着舰会导致前起落架载荷显著增大;直升机着舰下沉速度过大会导致着舰载荷急剧增大,可能会对结构造成破坏。     

基于双量程推力传感器的精确测力技术

针对双量程推力传感器在使用中测试精度低的问题,结合传感器固有特性,开展了传感器动态特性分析及误差补偿方法的研究。通过有限元分析和力锤冲击试验,结合结构分析获得了双量程力传感器等效二自由度和三自由度动力学模型。利用近似求积数值法对冲击力试验输出信号进行补偿,获得了接近标准信号的测试结果,对该补偿方法进行了有效性验证。结果显示:本方法对发动机试验的推力信号进行了补偿,推动了单室双推力发动机推力的精确测量,为双推力发动机的推力测试提供了有效途径。     

Quasi-biennial oscillations in the cross-correlation of properties of macrospicules

Jets, whatever small (e.g. spicules) or large (e.g. macrospicules) their size, may play a key role in momentum and energy transport from photosphere to chromosphere and at least to the low corona. Here, we investigate the properties of abundant, large-scale dynamic jets observable in the solar atmosphere: the macrospicules (MS). These jets are observationally more distinct phenomena than their little, and perhaps more ubiquitous, cousins, the spicules. Investigation of long-term variation of the properties of macrospicules may help to a better understanding of their underlying physics of generation and role in coronal heating. Taking advantage of the high temporal and spatial resolution of the Solar Dynamics Observatory, a new dataset, with several hundreds of macrospicules, was constructed encompassing a period of observations over six years. Here, we analyse the measured properties and relations between these properties of macrospicules as function of time during the observed time interval. We found that cross-correlations of several of these macrospicule properties display a strong oscillatory pattern. Next, wavelet analysis is used to provide more detailed information about the temporal behaviour of the various properties of MS. For coronal hole macrospicules, a significant peak is found at around 2-year period. This peak also exists partially or is shifted to longer period, in the case of quiet Sun macrospicules. These observed findings may be rooted in the underlying mechanism generating the solar magnetic field, i.e. the global solar dynamo.     

基于CFD动网格的内装式空射分离研究

研究了使用飞机发射运载火箭时的机箭分离过程.提出了一种可以解决内装式空射分离问题的整体解决方案,主要基于CAD三维实体建模方法、多体动力学方法和结合六自由度运动的计算流体力学(CFD)动网格方法.以CFD动网格计算为核心,进行了空射分离过程关键问题的研究,得到了火箭在载机气动干扰环境下的运动特性,为轨道卫星和弹道导弹的快速、廉价发射打下了研究基础.     

New insights into SNR evolution revealed by the discovery of recombining plasmas

We report the discovery of recombining plasmas in three supernova remnants (SNRs) with the Suzaku X-ray astronomy satellite. During SNR’s evolution, the expanding supernova ejecta and the ambient matter are compressed and heated by the reverse and forward shocks to form an X-ray emitting hot plasma. Since ionization proceeds slowly compared to shock heating, most young or middle-aged SNRs have ionizing (underionized) plasmas. Owing to high sensitivity of Suzaku, however, we have detected radiative recombination continua (RRCs) from the SNRs IC 443, W49B, and G359.1–0.5. The presence of the strong RRC is the definitive evidence that the plasma is recombining (overionized). As a possible origin of the overionization, an interaction between the ejecta and dense circumstellar matter is proposed; the highly ionized gas was made at the initial phase of the SNR evolution in dense regions, and subsequent rapid adiabatic expansion caused sudden cooling of the electrons. The analysis on the full X-ray band spectrum of IC 443, which is newly presented in this paper, provides a consistent picture with this scenario. We also comment on the implications from the fact that all the SNRs having recombining plasmas are correlated with the mixed-morphology class.     

高效图像资源管理器的设计与实现

针对数据存储量大引起的访问广域网服务器速度慢、不能对访问的客户进行细粒度的权限控制问题,研究了B/S模式下基于.NET平台的图像资源管理器的设计和实现技术。系统综合采用权限管理模型、动态加载、文档对象模型（DOM）等技术以及非点击无刷新伸缩控制方法,实现了图像资源管理器的分权限控制、高速访问以及无刷新高效联动等操作。实验验证了方法的可行性。     

某型直升机旋翼转速表的数字化设计方案

提出某型直升机数字旋翼转速表的研制方案,给出以频率/数字(F/D)变换电路为核心的主要硬件原理,分析了采样误差的产生及抑制误差的措施.装机部件研制成功证实了方案的可行性.     

具有动态发送功能的多信源认证码的构造

在一个群通信体系中,最基本并且最具有实际意义的认证系统是指关于动态发送者的多接收认证码(简称DMRA-code).但目前,许多学者对其研究仅仅局限于对一个信源的认证.然而在网络通信中,常常会有多信源传播的场景.基于这个问题,利用多项式构造一个具有动态发送功能的多信源认证码,并且验证了该模型的合理性以及计算出了可能的攻击概率,从而保证了所构造的方案的安全性.     

直升机燃油系统地面模拟试验中油面角的计算

油面角是直升机燃油系统地面模拟试验的主要模拟参数。如何确定油面角是试验的主要环节。本文介绍了直升机在不同飞行状态下的油面角的计算方法。     

直升机桨叶耐颗粒物/砂磨蚀标准分析

在分析研究直升机桨叶耐颗粒物/砂磨蚀标准主要技术要素的基础上,全面对比分析了MIL-STD-3033、ГОСТР52560-2006、GJB 1171-1991等国内外标准的基本内容,提出了装备研制及标准化工作相关建议。