Numerical Study of Turbulent Distribution and Noise Suppression in the Gas Turbine Engine Exhaust Pipe

• Main Authors: Chu-Hsiang Hung, 洪楚翔
• Other Authors: 吳文忠
• Format: Others
• Language: zh-TW
• Published: 2016
• Online Access: http://ndltd.ncl.edu.tw/handle/xrk3wb

碩士 === 國立虎尾科技大學 === 飛機工程系航空與電子科技碩士班 === 105 === In the requirements of the airport environment. At present the engine noise is one of the important factors affecting the environment, noise reduction equipment is necessary. The main noise of the engine is related to the degree of mixing of the discharged high-temperature high-speed jet with the external low-speed cold air. To reduce the noise, it is necessary to improve the mixing ratio of the internal flow and outside air. Therefore, this study discusses how to improve the appearance of the same exhaust area, which can achieve the same exhaust air volume and reduce the noise effect. In this study, CFD software Fluent was used for simulation. In order to improve its accuracy. First, the simulated and experimental data were compared for their sound pressure levels. After validation, a thrust eight-thousand-pound jet engine was used as the prototype design. And discuss the influence of three kinds of appearance changes. Have Wave, Chevron and Fold types. To investigate the distribution of appearance change after the tail section of the air flow turbulence and noise situation. The Chevron - type tail pipe has the best noise reduction effect. Noise reduction effect is about 8-13dB.