非对称变弹翼高速导弹气动特性计算与分析

通过不对称旋转左右弹翼的后掠角实现弹翼的不对称变化,利用飞行器快速计算软件Missile Datcom计算不同条件下导弹的气动参数.基于气动数据分析了后掠角非对称变化对升力、阻力、俯仰力矩及滚转力矩等气动特性的影响.通过分析可知,弹翼的不对称变形可显著的改变滚转力矩系数,将不对称变形的弹翼作为辅助控制机构,控制导弹的滚转运动,提高滚转运动的准确性和快速性.     

Tactile sensing and control of robotic manipulation

—This paper reviews the current state of the art and predicts the outlook in robotic tactile sensing for real-time control of dextrous manipulation. We begin with an overview of human touch sensing capabilities and draw lessons for robotic manipulation. Next, tactile sensor devices are described, including tactile array sensors, force-torque sensors, and dynamic tactile sensors. The information provided by these devices can be used in manipulation in many ways, such as finding contact locations and object shape, measuring contact forces, and determining contact conditions. Finally, recent progress in experimental use of tactile sensing in manipulation is discussed, and future directions for research in sensing and control are considered.     

基于变可信度模型差值的低可信度模型修正方法

为了解决优化设计中计算效率与高可信度信息获取之间的矛盾,从高、低可信度模型的物理机理出发,基于Kriging模型和拉丁超立方设计选样方法构造两模型差值的代理模型;并利用该代理模型对低可信度模型进行修正,构成了具有高可信度的修正模型.与直接对高可信度模型构造的代理模型相比,修正模型不但分析精度更高,而且所需的构造样本更小.文中分别以翼型气动力分析、机翼气动力分析和无人机隐身特性分析为例,从不同维数、不同学科的角度验证了修正模型特性,并进行了机理分析.     

变体机翼大变形梯形蒙皮结构研究

首先介绍了变体机翼及蒙皮结构的发展研究现状,提出了大变形梯形蒙皮结构的构想.随后,建立了梯形蒙皮结构的力学分析数学模型,与有限元仿真分析结果进行了比较和分析,验证了所建立数学分析模型的正确性,为进一步开展制备和实验研究奠定了理论基础.     

考虑机身干扰的机翼气动外形综合优化

由于受机身绕流的影响,后掠机翼翼根的流动非常复杂,翼根气动设计是后掠机翼气动设计的难点.本章发展了基于Kriging代理模型的双层粒子群优化算法,结合雷诺平均N-S方程流场求解器进行了考虑机身干扰的机翼气动外形综合优化研究,在保证机翼相对厚度和容积不减的前提下降低了气动阻力、低头力矩和翼根弯矩.而考虑非设计巡航状态的多...     

Creation and circuit implementation of two-to-eight–wing chaotic attractors using a 3D memristor-based system

This paper constructs a three-dimensional (3D) memristor-based system for creating multiwing chaotic attractors. A second-degree polynomial memristance function and a sixth-order exponent internal state memristor function with one parameter are employed, and the complexity of attractors is increased. A detailed analysis on dynamical behaviors of the proposed system are described, such as the bifurcation diagrams, finite-time local Lyapunov exponents, time series, phase portraits, and Poincaré maps. By adjusting the design parameters, the system displays two-to-eight–wing chaotic attractors, especially the five-wing and seven-wing attractors, which have never been found in the known systems. Further, we provide the calculation formula of the number of wings in the system, discuss the distribution of the involving inner holes on the plane, and design an electronic circuit to realize the proposed system. The experimental results of the circuit implementation agree with the numerical simulations on Matlab well. It indicates the potential engineering applications for various chaos-based information systems.     

二维机翼边界层的数值计算

直接在贴体自然坐标系下对二维水翼的边界层进行数值计算。边界层的数值求解采用了二种不同的方法(均用零方程模式来描述湍流应力),计算结果与实验数据吻合良好。     

瓦村水电站溢洪道体型优化试验研究

针对瓦村水电站溢洪道出口水流挑距过大、水舌空间扩散效果不佳、入水区域集中、泄洪消能效果差及泄槽内水翅现象严重等问题,采用比尺为1∶60的正态物理模型对溢洪道体型进行优化试验研究。结果表明,在闸墩尾部加设尾墩,使泄槽段水流流态有了极大的改善,水流平顺,基本上消除了水翅现象;采用连续燕尾挑坎使溢洪道出口水舌合理归槽,空中扩散效果良好,解决了入水集中的问题,消能效果较好,所提挑坎布置形式可供相关工程参考。     

热反应鸡粉、鸡肉膏及其在卤制品(盐焗鸡制品)中的应用

通过介绍热反应鸡粉、鸡肉膏的特点,以及他们的调味增香机理,通过比较拌合型香精特点,从盐焗鸡翅制品的产品风味等方面阐述了应用肉味调味料的必要性,利用富农产品天然、营养,耐高温等优势,通过盐焗鸡翅的生产工艺配方应用举例,确定热反应鸡粉、鸡肉膏在盐焗鸡翅制品中广泛的应用。