一种外部加翼的圆柱小目标声隐身结构设计

针对水下小型航行器日益增强的声隐身需求,基于菲涅耳(Fresnel)半波带理论,提出一种可提高目标声隐身性能的外部加翼结构。利用板块元方法计算并分析不同结构参数的优化翼型结构声隐身性能的提升效果。研究结果表明,外翼覆盖了圆柱散射贡献最大的半波带,加速相位变化,降低入射方向相同投影面积的散射贡献,使得圆柱正横方位的目标强度有效降低。当翼的开角为第一Fresnel半波带对应圆心角度且外翼与圆柱主体相切时,该结构在节约制造成本的同时可使声隐身性能的提升效果最好。文中进行了加翼模型声散射特性水池实验,优化结构的0°方位目标强度下降约7 dB,俯仰方向角检测概率显著降低,证明该类翼型结构可以有效提高目标声隐身性能。

基于环量场影响的Magnus风力机组合旋转圆型翼设计与研究

提出一种新型的面向Magnus风力机的组合旋转圆型(combined rotating cylinder,CRC)翼型设计思想,理论分析该翼型提高升力的作用机理;采用数值模拟计算方法研究该翼型的气动性能,将该翼型的数值模拟结果与传统翼型的试验结果作对比分析。结果表明:由于圆柱翼旋转产生的环量使得整个新型风力机翼型的环量得到较大提高,导致CRC翼型在马格努斯效应下产生的升力得到较大提高。表现为在整个攻角范围内的CRC翼型升力系数均远大于传统翼型,尤其是在低攻角范围内其升力系数约为传统翼型最大值的3倍,表明该翼型具有良好的价值。

An Experimental Study on Aerodynamic Sound Generated from Wake Interaction of Circular Cylinder and Airfoil with Attack Angle in Tandem

In our previous study, the effects of the interval between the cylinder and the airfoil on the aerodynamic sound were investigated and compared with the cases of single circular and single airfoil. In this study, the effects of the attack angle of the airfoil located downstream on the characteristics of aerodynamic sound and the wake structure are investigated at a given interval between the cylinder and the airfoil. It is found that the sound pressure level of DFN and the peak frequency decrease with increasing attack angle of airfoil because of the diffusive wake structure due to the increased back pressure of circular cylinder, which is caused by the blocking effect of airfoil. It is shown that the sound sources are corresponded to the attack points of shedding vortex form the upstream circular cylinder to the downstream airfoil. We conclude that the pressure fluctuation at the airfoil surface effects on the sound pressure level, from the flow visualizations and the exploration test of sound source.