积冰几何特性对翼型性能影响的神经网络预测

积冰几何形状对翼型气动系数的影响是复杂的.采用BP(Back Propagation)神经网络的LM(Levenberg-Marguardt)学习算法,建立明冰的典型几何特性(冰角前缘半径、冰角高度和冰角位置)对翼型气动系数影响的神经网络,得到该3种几何参数对气动系数影响的规律;建立了典型冰形参数对最大升力系数影响的神经网络,该网络能很好的预测冰形参数对应的最大升力系数值;此外,建立了冰型位置对舵面铰链力矩系数影响的神经网络.仿真结果表明,BP神经网络仿真结果与实验值具有高度一致性,并能预测非实验值条件下的气动系数;翼型表面积冰位置变化对气动系数影响最大;铰链力矩系数在失速迎角达到之前就发生突变,可以更安全地用来预测失速的发生.      

失调对叶片-轮盘耦合系统振动影响的预测

叶片 -轮盘系统的周期对称性经常由于制造、材料,以及非均匀磨损和其它因素而被破坏,引起系统出现失调现象,表现为结构特性的微小变化可能导致叶片振幅和响应的急剧增大。而失调也导致此类周期对称性结构振动特性计算的复杂化。利用有限元通用程序和模态综合技术,建立失调叶片 -轮盘耦合系统三维有限元模型,对一个有1 6个叶片的叶片 -轮盘耦合系统进行了振动特性计算分析,给出了叶片分散度和耦合度对振动特性的影响。     

基于ISA总线的高码速率大容量遥测数据存储器的研究

介绍基于 ISA(Industry Standard Architecture)总线的高码速度大容量遥测数据存储器的研究。作为计算机主存储设备的硬盘 ,它具有体积小 ,存储容量大的优点 ,本系统拟采用硬盘作为存储设备 ,且遥测数据在存储数据时采用脱线工作方式 ,我们设计了该存储器和计算机的接口且实现了对硬盘传输数据的 PIO(Program Input Output)方式的编程和对遥测数据的差错控制     

CFD simulation of helicopter rotor flow based on unsteady actuator disk model

Actuator Disks (AD) can provide characterizations of rotor wakes while reducing computational expense associated with modeling the fully resolved blades. This work presents an unsteady actuator disk method based on surface circulation distribution combined with empirical data, blade element theory and rotor momentum theory. The nonuniform circulation distribution accounts for 3D blade load effects, and in particular, tip loses. Numerical simulations were conducted for the isolated pressure sensitive paint model rotor blade in hover and forward flight using the HMB3 CFD solver of Glasgow University. Validation of CFD results in comparison with published numerical data was performed in hover, for a range of blade pitch angles using fully turbulent flow and the k-ω SST model. In forward flight, the vortex structures predicted using the unsteady actuator disk model showed configurations similar to the ones obtained using fully resolved rotor blades. Despite the reduced grid cells number, the CFD results for AD models captured well the main vortical structures around the rotor disk in comparison to the fully resolved cases.     

Composite profile of the Fe Kα spectral line emitted from a binary system of supermassive black holes

We used a model of a relativistic accretion disk around a supermassive black hole (SMBH), based on ray-tracing method in the Kerr metric, to study the variations of the composite Fe Kα line emitted from two accretion disks around SMBHs in a binary system. We assumed that the orbit of such a binary is approximately Keplerian, and simulated the composite line shapes for different orbital elements, accretion disk parameters and mass ratios of the components. The obtained results show that, if observed in the spectra of some SMBH binaries during their different orbital phases, such composite Fe Kα line profiles could be used to constrain the orbits and several properties of such SMBH binaries.     

FGH95粉末涡轮盘淬火过程计算机模拟

通过对PREP粉末as-HIP FGH95粉末涡轮盘和热等静压+包套锻造FGH95粉末涡轮盘固溶处理后盐浴淬火过程的计算机模拟,计算出不同取样位置的拉伸性能,与实测性能吻合较好.通过对应力场模拟得到盘件某些关键点的淬火应力情况,分析其开裂倾向,建议加大盘件不同尺寸截面的过渡圆弧,以减小应力集中.     

X-ray timing beyond the Rossi X-ray Timing Explorer

With its ability to look at bright galactic X-ray sources with sub-millisecond time resolution, the Rossi X-ray Timing Explorer (RXTE) discovered that the X-ray emission from accreting compact stars shows quasi-periodic oscillations on the dynamical timescales of the strong field region. RXTE showed also that waveform fitting of the oscillations resulting from hot spots at the surface of rapidly rotating neutron stars constrain their masses and radii. These two breakthroughs suddenly opened up a new window on fundamental physics, by providing new insights on strong gravity and dense matter. Building upon the RXTE legacy, in the Cosmic Vision exercise, testing General Relativity in the strong field limit and constraining the equation of state of dense matter were recognized recently as key goals to be pursued in the ESA science program for the years 2015–2025. This in turn identified the need for a large (10 m² class) aperture X-ray observatory. In recognition of this need, the XEUS mission concept which has evolved into a single launch L2 formation flying mission will have a fast timing instrument in the focal plane. In this paper, I will outline the unique science that will be addressed with fast X-ray timing on XEUS.     

MHD Spectroscopy of Transonic Flows

In previous publications (Keppens et al.: 2002, Astrophys. J. 569, L121; Goedbloed et al.: 2004a, Phys. Plasmas 11, 28), we have demonstrated that stationary rotation of magnetized plasma about a compact central object permits an enormous number of different MHD instabilities, with the well-known magneto-rotational instability (Velikhov, E. P.: 1959, Soviet Phys.–JETP Lett. 36, 995; Chandrasekhar, S.: 1960, Proc. Natl. Acad. Sci. U.S.A. 46, 253; Balbus, S. A. and Hawley, J. F.: 1991, Astrophys. J. 376, 214) as just one of them. We here concentrate on the new instabilities found that are driven by transonic transitions of the poloidal flow. A particularly promising class of instabilities, from the point of view of MHD turbulence in accretion disks, is the class of trans-slow Alfv’en continuum modes, that occur when the poloidal flow exceeds a critical value of the slow magnetosonic speed. When this happens, virtually every magnetic/flow surface of the disk becomes unstable with respect to highly localized modes of the continuous spectrum. The mode structures rotate, in turn, about the rotating disk. These structures lock and become explosively unstable when the mass of the central object is increased beyond a certain critical value. Their growth rates then become huge, of the order of the Alfv’en transit time. These instabilities appear to have all requisite properties to facilitate accretion flows across magnetic surfaces and jet formation.     

用于失谐叶盘动力学特性分析的减缩计算方法

提出了一种用于失谐叶盘动力学特性分析的减缩计算方法.该方法采用基于周期对称的谐波平衡法,建立非线性的迭代方程,能够基于单扇区的矩阵求解整个失谐叶盘的强迫响应,且不存在任何截断误差,因而效率高于部件模态综合法但精度并不降低.从周期对称结构理论出发给出了方法原理的数学推导,在此基础上通过一个失谐叶盘有限元模型算例对该方法的效率与精度进行了讨论.结果表明:相较部件模态综合法,周期对称谐波平衡法矩阵维度减小59.5%,计算复杂度减少93.4%,计算时间节省57.4%.     

预浸料厚坯超声切割工艺研究

 预浸料厚坯超声切割技术,具有无刀具磨损、加工速度快、加工精度高、无粉尘污染等优势,切割质量优异,在国外已得到了广泛应用,而国内目前仍处于初期研究阶段。本文以航空航天应用为主的碳纤维预浸料厚坯为实验材料,研究了切割温度、切割速度以及切割能量等切割工艺参数对切割质量的影响。研究结果表明,对于一定厚度的预浸料厚坯,最优的切割工艺参数组合:切割温度为5℃,切割速度为1.0 m/min,切割能量为8级。该研究方法与研究成果为超声切割技术在预浸料切割中的应用奠定了基础。