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Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges

机译：通过使用锯齿状叶片后缘降低风翼自噪声的风洞研究结果

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Dassen T.; Parchen R.; Bruggeman J.; Hagg F.;
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年度 1996
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正文语种 nl
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1. Poro-Serrated Trailing-Edge Devices for Airfoil Self-Noise Reduction [J] . Vathylakis Alexandros, Chong Tze Pei, Joseph Phillip F. AIAA Journal . 2015,第11期

机译：用于减小翼型自降噪的Poro锯齿形后缘设备
2. Estimation method to achieve a noise reduction effect of airfoil with a serrated trailing edge for wind turbine rotor [J] . Ryi Jaeha, Choi Jong-Soo Noise Control Engineering Journal . 2017,第4期

机译：估计方法实现翼型的降噪效果，具有风力涡轮机转子的锯齿状后缘
3. Airfoil Self-Noise Reduction by Gradient Distributed Porous Trailing Edges [J] . Wang Yong, Hao Nan-Song, Lu Xiang-Yu, Journal of aerospace engineering . 2021,第6期

机译：梯度分布式多孔尾部边缘翼型自降噪
4. Numerical Study on Noise Reduction of the Turbomachinery Blade Self-noise with Serrated Trailing Edge [C] . DUAN Wenhua, JI Liang, TONG Hang, AIAA/CEAS aeroacoustics conference . 2019

机译：锯齿形后缘涡轮叶片自降噪的数值研究
5. Wind Tunnel and Numerical Analysis of Thick Blunt Trailing Edge Airfoils [D] . McLennan, Anthony William 2010

机译：厚钝头后缘翼型的风洞和数值分析
6. Role of Polymeric Coating on Metallic Foams to Control the Aeroacoustic Noise Reduction of Airfoils with Permeable Trailing Edges [O] . Reza Hedayati, Alejandro Rubio Carpio, Salil Luesutthiviboon, 2019

机译：金属泡沫上的聚合物涂层在控制具有可渗透后缘的翼型的航空声降噪中的作用
7. Correction: Numerical Study on Noise Reduction of the Turbomachinery Blade Self-noise with Serrated Trailing Edge [O] . Wenhua Duan, Liang Ji, Hang Tong, 2019

机译：矫正：涡轮机械叶片自噪声噪声降低的数值研究，具有锯齿状后缘
8. Results of a Wind Tunnel Study on the Reduction of Airfoil Self-Noise by the211 Application of Serrated Blade Trailing Edges [R] . Dassen, T., Parchen, R., Bruggeman, J., 1996

机译：采用锯齿状叶片边缘211减少翼型自噪声的风洞研究结果

Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges

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