南京航空航天大学学报2024，Vol.56Issue(2)：264-272,9.DOI:10.16356/j.1005-2615.2024.02.008
火星六旋翼无人机旋翼气动外形稳健设计与优化
Robust Design and Optimization of Rotor Aerodynamic Shape of the Mars Hexacopter
宣金婷 1丁志伟 1赵洪 2李建波1
作者信息
- 1. 南京航空航天大学直升机动力学全国重点实验室,南京 210016
- 2. 中国直升机设计研究所,景德镇 333001
- 折叠
摘要
Abstract
Because of the extremely low density and low heat capacity of the Martian atmosphere,the atmospheric pressure and atmospheric density of Mars change greatly with temperature,which has strong uncertainty.The deterministic aerodynamic design of the rotor for a single atmospheric density may lead to a significant increase in the power consumption of the rotor at off-design points,affecting the normal use of the Mars helicopter.In order to avoid the above problems,this paper first studies of Martian atmospheric environment and establishes the probability distribution model of Martian atmospheric density.For the Mars hexacopter with greater application potential,the viscous vortex particle method is then used to establish a high-confidence refined rotor aerodynamic model in the Martian atmosphere,and the robust design optimization of the rotor aerodynamic shape is carried out by non-dominated sorting genetic algorithm Ⅱ.The designed rotor aerodynamic shape scheme maintains good aerodynamic performance in the face of Mars atmospheric density changes,and has stronger robustness,which is conducive to the Mars hexacopter to perform longer and longer Mars exploration missions in different atmospheric environments.关键词
火星/旋翼/气动优化/稳健设计/黏性涡Key words
Mars/rotor/aerodynamic optimization/robust design/viscous vortex分类
航空航天引用本文复制引用
宣金婷,丁志伟,赵洪,李建波..火星六旋翼无人机旋翼气动外形稳健设计与优化[J].南京航空航天大学学报,2024,56(2):264-272,9.
