尾流激励的叶片气动力降阶模型

气动力降阶模型是研究叶片气动弹性振动快速高效的新方法。现有气动力降阶模型的研究主要集中在叶片颤振方面，没有涉及更为常见的上游尾流激励的叶片振动问题。本文提出基于Volterra级数的尾流激励叶片气动力降阶模型，为尾流激励下叶片振动和动静叶干涉振动研究提供了新的思路。采用行波法简化尾流的参数个数，用阶跃信号法识别降阶模型的核函数。二维叶片的算例结果表明，本文方法可以较准确地描述尾流激励引起的叶片气动力振荡，而且计算效率极高。     

A door to model reduction in high-dimensional parameter space

Model reduction techniques such as Proper Generalized Decomposition (PGD) are decision-making tools that are about to revolutionize many domains. Unfortunately, their computation is still problematic for problems involving many parameters, for which one has to face the “curse of dimensionality”. An answer to this challenge is given in solid mechanics by the so-called “parameter-multiscale PGD”, which is based on Saint-Venant's principle. In this article, a model problem composed of up to a thousand parameters is presented, showing that the method is able to overcome the “curse of dimensionality”.     

一种高效的叶轮机叶片气动阻尼计算方法

运用叠加原理, 发展了一种可以运用于小振幅运动的叶 轮机叶片非定常气动力降阶模型, 并将该模型与传统的能量法相结合, 提出了一种叶轮机叶 片气动阻尼的高效求解方法. 运用该方法求解叶轮机叶片的气动阻尼系数, 对某个频率、某 个模态只需要进行一次非定常计算, 就可以求出所有叶间振动相角下的气动阻尼系 数, 提高了气动阻尼的求解效率. 在STCF4和NASA Rotor 67两个算例上运用非定常雷诺平均N-S(RANS)方程和提出的降阶模型进行了对比计算. 算例表明, 在小振幅下该方法的计算结果与RANS方程计算得到的气动阻尼系数能很 好地吻合, 而计算效率相比多通道非定常RANS方程计算提升了近一个数量级, 并且 该方法还可以运用于有失谐情况的颤振分析, 在工程上有较高的应用价值.     

无证书代理重签密方案

结合无证书密码体制和签密思想提出了一个无证书代理重签密方案,在方案中,使用一个半可信代理人实现了一个签密到另一个签密的透明转换.与其他相似方案相比,实现了签密的完全转换.一般情况下,在Alice的私钥和Bob的公钥下完成的签密经转换后只能用Alice的身份信息和Daddy的私钥解签密;在本文提出的方案中,由Alice的私钥和Bob的公钥完成的签密经转换后可以用Charlie的身份信息和Daddy的私钥解签密,且签密的验证不需要明文信息的直接参与.基于间隙双线性Diffie-Hellman问题,在随机预言机模型下,证明了可以抵抗无证书代理重签密中的第一类攻击.     

浮栅ROM器件辐射效应机理分析

分析了浮栅ROM器件的辐射效应机理，合理地解释了实验中观察到的现象.指出辐射产生的电子空穴对在器件中形成的氧化物陷阱电荷和界面陷阱电荷是导致存储单元及其外围电路出现错误的原因.浮栅ROM器件的中子、质子和⁶⁰Co γ辐射效应都是总剂量效应 . 关键词： FLASH ROM EEPROM 中子 质子 60Co γ')" href="#">⁶⁰Co γ 总剂量效应     

Evaluation of linear,inviscid, viscous,and reduced-order modelling aeroelastic solutions of the AGARD 445.6 wing using root locus analysis

Reduced-order modelling (ROM) methods are applied to the Computational Fluid Dynamics (CFD)-based aeroelastic analysis of the AGARD 445.6 wing in order to gain insight regarding well-known discrepancies between the aeroelastic analyses and the experimental results. The results presented include aeroelastic solutions using the inviscid Computational Aeroelasticity Programme–Transonic Small Disturbance (CAP-TSD) code and the FUN3D code (Euler and Navier–Stokes). Full CFD aeroelastic solutions and ROM aeroelastic solutions, computed at several Mach numbers, are presented in the form of root locus plots in order to better reveal the aeroelastic root migrations with increasing dynamic pressure. Important conclusions are drawn from these results including the ability of the linear CAP-TSD code to accurately predict the entire experimental flutter boundary (repeat of analyses performed in the 1980s), that the Euler solutions at supersonic conditions indicate that the third mode is always unstable, and that the FUN3D Navier–Stokes solutions stabilize the unstable third mode seen in the Euler solutions.     

弹性支撑圆柱绕流稳定性分析

基于CFD 技术,采用系统辨识方法,建立了亚临界雷诺数(Re < 47) 下绕圆柱流动的非定常气动力模型(reduced order model, ROM). 耦合结构运动方程和降阶气动力模型,建立了弹性支撑圆柱绕流的稳定性分析模型. 算例分析了亚临界雷诺数下,结构固有频率、质量比等参数以及支撑方式对弹性系统稳定性的影响. 对于单自由度横向支撑圆柱,当结构固有频率趋近流动最不稳定模态频率时,弹性系统会在一定频率范围内失稳,这种现象最低可在Re~20 时出现. 旋转自由度的释放能够进一步降低系统的稳定性,可将临界雷诺数进一步降低至18 左右. ROM 方法不仅具有很高的效率,而且清晰地指出了弹性系统失稳的根本原因:流动模态和结构模态耦合作用导致结构模态失稳所致. 因此,失稳状态下系统振荡频率锁定于结构固有频率. 基于ROM 技术预测的失稳边界与直接CFD/CSD 仿真结果吻合,证明了该方法的正确性和精度.     

Experimental study on radiation effects in floating gate read-only-memories and static random access memories

Radiation effects of the floating gate read-only-memory （FG ROM） and the static random access memory （SRAM） have been evaluated using the 14 MeV neutron and 31.9MeV proton beams and Co-60 γ-rays. The neutron fluence, when the first error occurs in the FG ROMs, is at least 5 orders of magnitude higher than that in the SRAMs, and the proton fluence, 4 orders of magnitude higher. The total dose threshold for Co-60 γ-ray irradiation is about 104 rad （Si） for both memories. The difference and similarity are attributed to the structure of the memory cells and the mechanism of radiation effects. It is concluded that the FG ROMs are more reliable as semiconductor memories for storing data than the SRAMs, when they are used in the satellites or space crafts exposed to high energy particle radiation.     

发动机流道气动分析的上下游边界替代降阶模型

为了解决航空发动机流道内上下游干涉带来的计算量大的问题,提出了一种边界替代降阶模型方法。该方法辨识出研究流域与相邻的上下游流域交界面的气动力降阶模型,并耦合到该研究流域仿真模型的交界面上,用以表征上下游对该流域的影响,由此将多流域计算转化为单流域计算,同时又考虑了上下游的影响。采用一阶Volterra级数降阶模型实现了该方法。结果表明,采用本文方法和所有流域都采用CFD得到的压力和速度一致;本文方法所用的网格更少,可以加速收敛和提高计算速度。     

Convergence acceleration of continuous adjoint solvers using a reduced‐order model

A novel acceleration technique using a reduced‐order model is presented to speed up convergence of continuous adjoint solvers. The acceleration is achieved by projecting to an improved solution within an iterative process solely using early solution results. This is achieved by forming basis vectors from early iteration adjoint solutions to perform model order reduction of the adjoint equations. The reduced‐order model of the adjoint equations is then substituted into the full‐order discretized governing equations to determine weighting coefficients for each basis vector. With these coefficients, a linear combination of the basis vectors is used to project to an improved solution. The method is applied to 3 inviscid quasi‐1D nozzle flow cases including fully subsonic flow, subsonic inlet to supersonic outlet flow, and transonic flow with a shock. Significant cost reductions are achieved for a single application as well as repeated applications of the convergence acceleration technique.