空气动力学学报2018，Vol.36Issue(3)：372-384,409,14.DOI:10.7638/kqdlxxb-2017.0159
大型客机增升装置噪声机理与噪声控制综述
Review of the mechanism and noise control of high-lift device noise
摘要
Abstract
High-lift device noise has been identified as a major noise source during aircraft approach and landing.Reviews on the noise generation mechanism and noise control methods of the high-lift device noise are conducted.Challenges in understanding the physical mechanism of the noise generation and implementing effective noise control has been pointed out.We performed high-fidelity large-eddy simulations for flow past the slat,flap trailing-edge and flap side-edge separately.Based on phase-averaging analysis,proper orthogonal decomposition (POD),dynamic mode decomposition (DMD),and two-point correlations,we increase insights on the underlying physics of the high-lift device noise.The results are expected to guide the design of high efficient noise control approaches.关键词
增升装置噪声/噪声机理/噪声控制Key words
high-lift device noise/noise generation mechanism/noise control methods分类
数理科学引用本文复制引用
李伟鹏..大型客机增升装置噪声机理与噪声控制综述[J].空气动力学学报,2018,36(3):372-384,409,14.基金项目
国家自然科学基金(11772194) （11772194）
国家"973"课题(2014CB744802,2014CB744804) （2014CB744802,2014CB744804）
