Yong WANG, Nansong HAO, Qingren LAI, et al. Experiment of rod⁃airfoil interaction noise reduction using porous leading edges[J]. Journal of Aerospace Power, 2022, 37(9): 1807-1814.
DOI:
Yong WANG, Nansong HAO, Qingren LAI, et al. Experiment of rod⁃airfoil interaction noise reduction using porous leading edges[J]. Journal of Aerospace Power, 2022, 37(9): 1807-1814.DOI: 10.13224/j.cnki.jasp.20210313.
Experiment of rod⁃airfoil interaction noise reduction using porous leading edges
为了抑制圆柱⁃翼型干涉噪声,提出了仿生多孔前缘结构的降噪措施,并在0.55 m×0.4 m声学风洞中进行了实验验证。针对典型构型,对比确定了多孔金属泡沫降低圆柱⁃翼型干涉峰值噪声和中高频噪声的效果。3种不同ppi(pores per inch)值多孔金属泡沫的详细声学测量结果表明,所提出的多孔前缘结构能在翼型迎角为0°和10°时,分别降低最多4.10 dB和4.67 dB的圆柱⁃翼型干涉峰值噪声,且能明显降低峰值频率右侧的中高频噪声;多孔材料的占比越大、ppi值越小,整体降噪效果越好。
Abstract
A method for rod⁃airfoil interaction noise reduction with a bio⁃inspired porous leading edge structure was proposed,and then verified experimentally in the 0.55 m×0.4 m acoustic wind tunnel.For typical configurations,the effects of porous metal foams in reducing the peak noise and the mid⁃to⁃high frequency noise of the rod⁃airfoil interaction were determined.The detailed acoustic measurements on three porous metal foams with different ppi (pores per inch) values showed that the proposed porous leading edges can reduce the peak value of the rod⁃airfoil interaction noise by up to 4.10 dB and 4.67 dB at the airfoil angle of attack of 0° and 10°,respectively.It can also significantly reduce the mid⁃to⁃high frequency noise on the right side of the peak frequency.The larger the proportion,the smaller the ppi value of the porous materials and the better the overall noise reduction effect.
关键词
Keywords
references
CASALINO D , JACOB M , ROGER M . Prediction of rod⁃airfoil interaction noise using the Ffowcs⁃Williams⁃Hawkings analogy [J]. AIAA Journal , 2003 , 41 ( 2 ): 182 ⁃ 191 .
HENNING A , KOOP L , EHRENFRIED K . Simultaneous particle image velocimetry and microphone array measurements on a rod⁃airfoil configuration [J]. AIAA Journal , 2010 , 48 ( 10 ): 2263 ⁃ 2273 .
WANG Yong , ZHAO Kun , LU Xiangyu , et al . Bio⁃inspired aerodynamic noise control:a bibliographic review [J]. Applied Scicences , 2019 , 9 ( 11 ): 2224.1 ‑ 2224.43 .
JACOB M C . BOUDET J,CASALINO D, et al.A rod⁃airfoil experiment as benchmark for broadband noise modeling[J]. Theoretical and Computational Fluid Dynamics , 2005 , 19 : 171 ⁃ 196 .
AGRAWAL B R , SHAMA A . Aerodynamic noise prediction for a rod⁃airfoil configuration using large eddy simulations [R]. Atlanta,US : 20th AIAA/CEAS Aeroacoustics Conference , 2014 .
GIRET J , SENGISSEN A , MOREAU S , et al . Noise source analysis of a rod⁃airfoil configuration using unstructured large⁃eddy simulation [J]. AIAA Journal , 2015 , 53 ( 4 ): 1062 ⁃ 1077 .
CARAENI M , DAI Y , CARAENI D . Acoustic investigation of rod airfoil configuration with DES and FWH [R]. AIAA⁃2007⁃4106 , 2007 .
GALDEANO S , BARRÉ S , RÉAU N . Noise radiated by a rod⁃airfoil configuration using DES and the Ffowcs⁃Williams & Hawkings' analogy [R]. Stockholm,Sweden : 16th AIAA/CEAS Aeroacoustics Conference , 2010 .
XIE Ke , LI Xiaodong , LIN Dakai . An experimental investigation of the flow field of rod⁃airfoil interaction [J]. Aircraft Design , 2009 , 29 ( 4 ): 6 ⁃ 12 . (in Chinese)
GIESLER J , SARRADJ E . Measurement of broadband noise generation on rod⁃airfoil⁃configurations [R]. AIAA⁃2009⁃3308 , 2009 .
LIU Xingqiang , HUANG Wenchao , LI Hongli , et al . The simulation for rod⁃airfoil interaction noise [J]. Science Technology and Engineering , 2017 , 17 ( 9 ): 278 ⁃ 283 . (in Chinese)
LI Yong , WANG Xunnian , CHEN Zhengwu , et al . Experimental study of vortex⁃structure interaction noise radiated from rod⁃airfoil configurations [J]. Journal of Fluids and Structures , 2014 , 51 : 313 ⁃ 325 .
SILLER H A , JACOB M C , MICHEL U . Flow and noise modification by suction and blowing on a rod⁃airfoil configuration [R]. AIAA⁃2005⁃3029 , 2005 .
SIOZOS⁃ROUSOULIS L , GHORBANIASL G , LACOR C . Noise control by a rotating rod in a rod⁃airfoil configuration [R]. AIAA⁃ 2015⁃2826 2015.
CHEN Weijie , WANG Xunnian , QIAO Weiyang , et al . Rod⁃airfoil interaction noise reduction using leading edge serrations [R]. AIAA⁃2015⁃3264 , 2015 .
CHEN Weijie , QIAO Weiyang , TONG Fan , et al . Experimental investigation of wavy leading edges on rod⁃aerofoil interaction noise [J]. Journal of Sound and Vibration , 2018 , 422 : 409 ⁃ 431 .
ROGER M , SCHRAM C , DE SANTANA L . Reduction of airfoil turbulence⁃impingement noise by means of leading⁃edge serrations and/or porous materials [R]. AIAA⁃2013⁃2108 , 2013 .
WANG Yong , HAO Nansong , GENG Zihai , et al . Measurements of circular cylinder's wake using time⁃resolved PIV [J]. Journal of Experiments in Fluid Mechanics , 2018 , 32 ( 1 ): 64 ⁃ 70 . (in Chinese)
LIU Y , DOWLING A P , SHIN H C , et al . Experimental study of surface roughness noise [R]. AIAA⁃2007⁃3449 , 2007 .