高超声速钝楔边界层转捩大涡模拟

 以五阶迎风和八阶对称格式混合差分格式求解三维可压缩滤波Navier-Stokes方程,对来流Mach数为6.0、半锥角5°的高超声速空间发展钝楔边界层转捩至完全湍流进行了大涡模拟。时间推进采用紧致存储三阶Runge-Kutta方法,亚格子尺度模型为Driest因子修正的Smagorinsky涡黏性模型。通过定常流场入口边界附近吹／吸引入不稳定扰动斜波的方法数值模拟得到了层流失稳转捩直至完全湍流的空间发展全过程。对扰动的线性、非线性增长以及湍流斑的形成和发展进行了分析,给出了转捩及完全湍流下的速度相关量统计并与实验、DNS结果进行了对比分析,计算结果与理论及实验吻合。     

Simulation and Analysis of Crashworthiness of Fuel Tank for Helicopters

Crashworthiness requirement of fuel tanks is one of the important requirements in helicopter designs. The relations among the protection frame, textile layer and rubber layer of the fuel tank are introduced. Two appropriate FE models are established, one is for an uncovered helicopter fuel tank without protection frame, and the other is for fuel tank with protection frame. The dynamic responses of the two types of fuel tanks impinging on the ground with velocities of 17.3 m/s are numerically simulated for the purpose of analyzing energy-absorbing capabilities of the textile layer and protection frame. The feasibility of the current crashworthiness design of the fuel tank is examined though comparing the dynamic response behaviors of the two fuel tanks.     

A novel strategy for fine-grained semantic verification of civil aviation radiotelephony read-backs

During the flight of the aircraft, the pilot must repeat the instruction sent by the controller, and the controller must further confirm these read-backs, in this way to further ensure the safety of air transportation. However, fatigue, tension, negligence and other human factors may prevent the controller from realizing read-back errors in time, which is a huge hidden danger for the safety of civil aviation transportation. This paper proposes a novel strategy to implement fine-grained semantic ...     

Assessment and improvement of k-ω-γ model for separation-induced transition prediction

The purpose of this work is to improve the k-ω-γ transition model for separationinduced transition prediction. The fundamental cause of the excessively small separation bubble predicted by k-ω-γ model is scrutinized from the perspective of model construction. On the basis,three rectifications are conducted to improve the k-ω-γ model for separation-induced transition.Firstly, a damping function is established via comparing the molecular diffusion timescale with the rapid pressure-strain timescale...     

新电位移边界条件下的压电介质断裂问题

应用边界元法,并结合一种特殊的复变函数基本解,研究了压电介质的断裂问题。由于该基本解完全遵循本构方程没有对电位移边界作假设,所以结论同非穿透性裂纹假设的结果有较大差异。通过计算表明,外加力载荷不但会引起裂纹尖端应力奇异性,也会引起电场奇异性,同样,外加电压也会引起裂纹尖端应力奇异性。     

三维编织复合材料圆柱壳轴压下的屈曲分析

根据边界层理论,采用奇异摄动法,考虑非线性前屈曲、大挠度和初始几何缺陷的影响,分析在固支条件下,三维四向编织复合材料圆柱壳在轴压下的屈曲和后屈曲性态,讨论了纤维体积含量、几何参数等因素对圆柱壳屈曲的影响.结果表明,纤维体积含量、编织角和初始缺陷对编织复合材料圆柱壳的影响是不可忽视的.     

用电磁体积力的翼型绕流控制实验研究

研究了电磁体积力控制弱电解质溶液流动边界层的基本原理以及分析了翼型电磁激活板的绕流实验结果.电磁体积力控制弱电解质溶液流动边界层是磁场和电流相互作用产生电磁体积力作用在流体上的结果.实验结果表明:电磁力作用改变了翼型表面的流体边界层的结构,其作用与改变翼型的迎角类似.加正向电磁力,相当于减小翼型的迎角,可以抑制流动分离,消除涡街;而反向电磁力则相当于增大迎角,在翼型的背风面产生大尺度的流动分离,流场中出现复杂的旋涡结构.     

含孔边裂纹各向异性有限板的二维问题

应用边界元法,并结合一种特殊的复变函数基本解,研究了含孔边裂纹的各向异性有限板的应力强度因子修正系数的计算。这种特解边界元法避免了在裂纹附近划分单元,可以获得较好的数值计算精度。通过算例分析,结果表明本方法精度高,运算量小,具有一定的工程应用价值。     

体育场挑蓬风荷载模拟实验研究

能容纳五万多观众的浙江省黄龙体育中心主体育场,在观众席上建有能遮挡风雨的挑蓬,挑蓬之大达座席覆盖率９０％以上,总面积２１０００ｍ２。挑蓬被支撑在外环梁和由斜拉索吊拉的内环梁上。大跨度梁结构受力问题,是建筑结构业一个十分复杂的问题,而杭州地区的地理位置处于我国的台风区,更显出风荷载影响的严重性。因此需对体育场置于大气边界层风洞中进行风荷载模拟实验,以取得合理的挑蓬体型系数,为结构设计的合理性和可靠性提供重要依据。最终可以节省建筑物的造价。     

褶皱结构成形时的形状偏差计算

解决了褶皱结构成形时相邻的平行四边形平面元素之间连接区棱的修圆半径值预测问题。把毛坯模拟成薄板，定义了平行四边形平面元素的边界条件，采用能量法导出挠度和力函数的非线性微分方程组，利用积分－差分法实现其数值解，并提供计算结果和分析应力－应变场。采用的计算方法可用于研究毛坯的刚度参数和工艺参数对褶皱结构的形状影响。