Raffel Markus, Bauknecht André, Ramasamy Manikandan, Yamauchi Gloria K, Heineck James T, Jenkins Luther N
AIAA J. 2017 Sep;55(9):2859-2874. doi: 10.2514/1.J055571. Epub 2017 Jun 2.
The advancement of flow measurement techniques continues to extend experimental boundaries and thus significantly contributes to improving our understanding of both basic and applied aerodynamics. This is particularly apparent in the case of particle image velocimetry (PIV), where its application has furthered the existing knowledge in several areas of helicopter rotor aerodynamics. The complex nature of helicopter rotor flows presents unique challenges to experimentalists, including transonic flow, concentrated vortices and dynamic stall. To illustrate the impact of the technological advancements on the way helicopter aerodynamics is studied today, the development of PIV since the early nineties of the last century is reviewed and some recent PIV applications are described. Using examples of main rotor wakes, dynamic stall and flow control investigations, the capabilities of large-scale, time-resolved and volumetric PIV are summarized.
流动测量技术的进步不断拓展实验边界,从而极大地有助于增进我们对基础和应用空气动力学的理解。这在粒子图像测速技术(PIV)的情况下尤为明显,其应用推动了直升机旋翼空气动力学多个领域的现有知识发展。直升机旋翼流的复杂特性给实验人员带来了独特的挑战,包括跨音速流、集中涡和动态失速。为了说明技术进步对当今直升机空气动力学研究方式的影响,回顾了自上世纪九十年代初以来PIV的发展,并描述了一些近期的PIV应用。通过主旋翼尾流、动态失速和流动控制研究的例子,总结了大规模、时间分辨和体积PIV的能力。