抗阵风载荷的小型无人飞行器设计及相关风洞舵效比较

本文目的在于探索验证微小型飞行器的气动布局与抗突风载荷能力的关系,结合风洞试验验证了结果并进行了数据分析。在低雷诺数条件下采用大边条、小展弦比非常规的气动布局设计,根据性能指标要求对飞行器的机翼面积、翼展、翼型等相关参数进行了分析设计;运用数值模拟等手段对全机简化模型进行了气动力计算,对结果进了行初步的定性分析,为初始的设计提供了验证;结合实际的靶机制作得到了实际飞机的风洞验证缩比模型,对其进行了风洞的常规测力实验。根据风洞试验结果对飞机升降舵舵面与副翼舵面偏转0°、±15°、±30°的气动性能进行了评估,为进一步的理论分析提供依据。结合实际外场飞行实验情况得出飞行器的实际气动性能,并对大量相关风洞试验数据进行了分析;探索性地给出了一条适用于微小型飞行器进行的新设计方法和设计流程,为设计适应于阵风载荷等恶劣气候条件下微小的型飞行器提供了参考新思路。     

基于风洞试验的不同坡度多跨锯齿屋面风压特性研究

多跨锯齿屋面因其具有跨度大、结构轻盈的特点成为典型的风灾易损结构。目前国内规范对锯齿屋盖的风荷载规定较为粗略,简单给定了统一的风压系数参考值,在实际工程应用中具有一定的局限性。本文以某4跨锯齿房屋为研究对象,通过风洞试验测试了15°、21°、26°、30°和40°等5种不同屋面坡度对锯齿屋盖风压特性的影响。试验结果表明,我国建筑结构荷载规范GB 50009-2012关于锯齿屋面的负风压系数绝对值明显偏小,锯齿屋面最不利均面积负风压系数随着坡度的增加逐渐从高屋角(HC)区转移到屋面边区(SE),且与HC区相反,SE区内的最不利负风压系数绝对值随角度增加而增大;锯齿中间B、C跨最不利均面积负风压系数始终出现在HE区,其绝对值随角度增加而增大,而尾跨D则出现在SE区,且随角度增加而减小;屋面最不利极值负风压系数为-9.6,随着屋面坡度的增大,屋面的最大极值负风压系数绝对值逐渐减小。此外,以各坡度屋面负风压系数的分布为依据,给出了不同屋面坡度范围和不同跨屋面风压系数分区划分建议。     

Principle of temperature,velocity and pressure of upper atmospheric wind measurement for the Voigt profile

Using the accurate expression of the Fourier transform of the pure Voigt spectral line profile, we present the principle of the passive optical method to measure temperature, velocity, and pressure of atmospheric wind for the Voigt profile. Through discussion, from the Gaussian, Lorentzian and Voigt profiles, we find that velocity will not be affected, pressure can be derived for Lorentzian and Voigt profiles, and temperature will be affected greatly. By simulation and comparison, we find that temperature derived from the Voigt profile is greater than that from the Gaussian profile, and it is less than that from the Lorentzian profile. This discussion will be significant in accurate upper atmospheric wind measurement.     

Infrared study of hydrogen up to 310 GPa at room temperature

We observed a strong difference of the pressure dependence of the infrared (IR) active molecular vibron of hydrogen in phase IV in the 200–310 GPa pressure range in comparison with the Raman vibrons. While the Raman vibron strongly splits (～250 cm^?1) at the transition from phases III to IV at 220 GPa, the IR vibron nearly does not change. This small spitting of IR vibron is not described by the graphene-like structure proposed for phase IV. The combined pressure dependence of Raman and IR vibrons provides a sensitive test for further theoretical models of phase IV.     

High-pressure route to superhard boron-rich solids

Novel superhard phases are expected to be found among various high-pressure polymorphs of light element compounds. Besides diamond-like phases, the icosahedral boron-rich solids are of particular interest because they could combine high hardness with advanced electronic and phonon transport properties, lightness, high thermal and chemical stability. Here we review some recent results on high-pressure synthesis of novel boron-rich solids.     

Using a pseudo-functionally graded interlayer in order to improve the static and dynamic behavior of wind turbine blade T-bolt root joints

The large wind turbines blades with multi-ton composite structures are mostly connected to the peach-bearings flanges using T-bolt joints which induce shear and bearing stress fields around the cross bolts. The significant differences between the modulus of elasticity of metallic bolts and composite surrounding materials cause stress concentration around interfaced zones and, also, limit the load capacity of the joints. In the present research, a pseudo functionally graded material (PFGM) as an interlayer is used around the cross bolts to examine the reduction of the stress concentration. Some radial variation of the mechanical properties would be considered for this interlayer. The finite element method is used to analyze the structures. Loadings are applied to the center of the cross bolts analogous to the real cases. Both the static and dynamic loadings are studied. For the finite element of the functionally graded material interlayer, a multilayer alternative material with constant properties in each layer is used. The results show that using an isotropic single layer with an average modulus of elasticity and specific thickness decreases the stress concentration of the composite part up to 47%. The various property models for the interlayer also show that an appropriated model can decrease the stress concentration up to 55%. Dynamic transient analyses would be implemented over the joint structure and improved considering to the practical cases. Using the PFGM interlayer decreases the constant and variable parts of the stresses up to 55% and also causes significant increasing of the joint fatigue life.     

超短时延测量DFB激光器的动态线宽

激光器调谐过程中的动态线宽是非常重要的参数, 然而, 当前各种测量方法得到的都是激光器稳定状态下的静态线宽. 本文提出一种对干涉拍信号进行基于局部均值分解的时频分析进而获取激光动态线宽的方法, 通过仿真信号验证了这种时频分析方法提取瞬时相位噪声的有效性; 构建实验系统, 利用10cm路径差产生约0.5ns的超短时延, 提取相位噪声的时频分布, 首次得到了分布反馈半导体激光器在脉冲工作模式下的动态线宽. 关键词： 超短时延 动态线宽 局部均值分解 时频分布     

使用叠栅层析技术测量超音速风洞中的非对称复杂密度场

使用叠栅层析技术解决超音速风洞中复杂密度场的测量难题。应用高灵敏度叠栅偏折仪和间隔角度旋转模型的方法获取超音速风洞中流场的多方向叠栅条纹图。层析计算中使用一种新的偏折角修正迭代的叠栅层析算法,该方法可以实现对有限角采样和包含遮挡物的非完全数据重建,迭代过程中结合内边界平滑滤波提高重建精度。实验中获取了马赫数为2.52的超音速风洞中9幅不同采样角的条纹图,经过50次迭代计算后重建出膨胀波区非对称密度场的截面分布,并对测量结果和误差进行了分析和讨论。使用计算流体力学技术对该密度场进行建模和计算,验证了叠栅层析重建结果的正确性,证实了该技术在测量复杂流场领域的重要价值。     

The relevance of pressure-sensitive paint to aerodynamic research

Aerodynamic tests are designed to give information about the performance of a model when subjected to an airflow. The introduction of pressure sensitive paint provides a new method for obtaining the pressure distribution on the surface of wind-tunnel models. A paint, the luminescence of which is dependent on air pressure, is applied to the surface of the model and the pressure distribution is obtained from the image produced. This paper gives an explanation of this technique, a résumé of possible applications and some results from research performed at DRA Bedford.     

自适应光学对大气扰动波前的补偿效果研究：I.理论推导

在采用冻结湍流假设和几何光学近似的条件下，得到了经自适应光学系统校正后的剩余波前相位扰动的结构函数，进而根据剩余相位结构函数与系统Ｓｔｒｅｈｌ比的关系，求出自适应光学系统的补偿效果受系统的时空传递函数，大气湍流，光波传播路径上的横向风，观察目标的旋转角速度以及系统时间延迟影响情况的解析表达式。