Bluff-body aerodynamic drag and noise reduction
Last updated on April 6, 2022
Aerodynamic and aeroacoustic characteristics of a cylinder with longitudinal grooves were studied in an anechoic wind tunnel, emphasizing on drag and noise attenuation. The parallel mounted load cells and a single microphone measured the aerodynamic resistance and noise of a circular cylinder with longitudinal grooves at Reynolds number ranging from 5:84 _ 104 to 8:48 _ 104, covering the flow regimes from the sub-critical to the post-critical states. The results show that longitudinal grooves can effectively trigger the boundary-layer transition started at a Reynolds number around 5:84 _ 104, causing the so-called drag crisis. During the transition process, a drag reduction over 50% and a maximum noise attenuation over 15 dB can be achieved
Reference
Chuntai Zheng, et al., An experimental investigation of drag and noise reduction from a circular cylinder using longitudinal grooves., Physics of Fluids, 33, 115110, 2021.