Computational study of flow incidence effects on the aeroacoustics of low blade-tip Mach number propellers

标题
Computational study of flow incidence effects on the aeroacoustics of low blade-tip Mach number propellers
作者
关键词
Lattice-Boltzmann method, Propeller, Drone, Yaw angle, Aerodynamics, Aeroacoustics
出版物
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 120, Issue -, Pages 107275
出版商
Elsevier BV
发表日期
2021-12-08
DOI
10.1016/j.ast.2021.107275

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