坡面浅层明流流态界定方法之商榷

为了探求坡面薄层水流流态界定方法,从流体力学与泥沙运动学观点出发,对4种不同粗糙尺度床面（光滑玻璃、人工加糙粒径分别为0．075、0．245和0．380mm）、5种不同坡度下坡面薄层水流放水进行试验研究,并对薄层水流阻力规律与明渠水流阻力规律进行了比较分析。在此基础上提出了粘性底层厚度与水深之比作为新的无量纲临界判数,结果表明该判数能更好地反映坡面薄层水流流动型态。     

表面粘贴光纤光栅传感器的应变传递分析

光纤光栅传感器粘贴于航空结构的基体表面后,基体结构的真实应变与光纤光栅传感器测得的应变之间存在一个传递系数。本文根据应用环境,建立了＂基体结构—胶粘体—光纤传感器＂的应变传递简化模型,推导了裸光纤光栅传感器测得的应变与结构基体实际应变的比值,即应变传递率,并对影响传递率的各种参数进行分析和模拟,根据实际条件得到了粘贴的最佳参数。     

区间贝齐尔曲面的逼近(英文)

根据摄动理论,提出一种使用最小能量法的区间贝齐尔曲面逼近有理曲面的方法。该方法采用了恰当的范数,可以对摄动曲面以较多的限制,并通过实例演示了该方法的应用。实验可以与细分技术相结合,得到有理曲面的分片区间多项式的逼近。     

具有随机不确定性的机翼颤振优化

针对不确定性参数在颤振优化分析中的影响,提出了一种含颤振约束的、具有随机不确定性的机翼气动弹性优化设计方法.在MSC.NASTRAN平台上建立了结构的动力学模型、采用ZAERO程序进行了非定常气动力计算与颤振分析,用响应面方法计算了隐式失效功能函数,以重量最小为设计目标,对包含颤振概率约束的复合材料机翼进行了优化设计....     

Plasmasphere Response: Tutorial and Review of Recent Imaging Results

The plasmasphere is the cold, dense innermost region of the magnetosphere that is populated by upflow of ionospheric plasma along geomagnetic field lines. Driven directly by dayside magnetopause reconnection, enhanced sunward convection erodes the outer layers of the plasmasphere. Erosion causes the plasmasphere outer boundary, the plasmapause, to move inward on the nightside and outward on the dayside to form plumes of dense plasma extending sunward into the outer magnetosphere. Coupling between the inner magnetosphere and ionosphere can significantly modify the convection field, either enhancing sunward flows near dusk or shielding them on the night side. The plasmaspheric configuration plays a crucial role in the inner magnetosphere; wave-particle interactions inside the plasmasphere can cause scattering and loss of warmer space plasmas such as the ring current and radiation belts.     

航天产品深孔加工技术综述

在航空航天制造业中，深孔加工技术是一项仍在发展的综合技术。深孔加工是处于封闭或半封闭状态下进行的，加工难度主要体现在精加工工序上。深孔加工分为内排屑和外排屑两大类，不同的工艺选用不同的排屑方式。本文作者对难切削材料、深孔精密加工，加工实时监测进行了介绍，探讨了该领域的研究动向。     

Numerical investigation on adiabatic film cooling effectiveness and heat transfer coefficient for effusion cooling over a transverse corrugated surface

Three-dimensional numerical computations are conducted to investigate the effects of the blowing ratio and corrugation geometry on the adiabatic film cooling effectiveness as well as the heat transfer coefficient over a transverse corrugated surface. It is noticeable that the adiabatic wall temperature on the wavy valley of the transverse corrugated surface is relatively lower than that on the wavy peak. Surface corrugation has a relatively obvious influence on the laterally-averaged adiabatic film cooling effectiveness in the region where the effusion film layer is developed, but has little influence in the front region. Compared to a flat surface, the transverse corrugated sur-face produces a smaller adiabatic film cooling effectiveness and a higher heat transfer coefficient ratio. The effusion cooling difference between the flat and corrugated surfaces behaves more obvi-ously under a small aspect ratio of the wavy corrugation.     

双摆线滚子行星传动

双摆线滚子行星传动是一种新型的传动装置。它具有传动比范围大、结构紧凑、承载能力大、效率高等优点。文中对其啮合原理、方案设计和传动比计算进行了初步的探讨。     

飞机静压系统导管内径的优选

推导出静压系统迟滞指标植与结构参数的关系式，指出减小迟滞指标值的最有措施是增大导管的内径。同时阐述了迟滞的成因及其对飞机的负效应。     

发展用于高速飞行器前体/进气道匹配设计的逆特征线法

发展了一个可以在给定激波形状的条件下得到相应型面的逆特征线法,解决了前人方法求解鲁棒性和精度差的问题.对于一个非均匀超声速来流下给定形状的激波,该方法可求解出能生成该激波的气动型面及依赖域流场.数值校验表明:在马赫数为5的来流条件下逆特征线法按给定的圆锥激波计算的圆锥形状(锥顶角)相对误差小于0.5‰;通过两级轴对称激波的流场校验计算,可精准地求解出对应于此流场的两级外压缩圆锥.应用该方法设计了3个气动问题的造型:具有两级激波的Bump型面、马赫数为4的乘波前体以及乘波前体与进气道一体化造型.流场CFD计算结果显示这些造型设计效果良好,说明该逆特征线法可为这些问题的提供了一种途径.