海军航空工程学院学报2011，Vol.26Issue(4)：365-369,5.
桨叶结冰对尾桨气动性能的影响
Influence of Blade Icing on the Aerodynamic Performance of a Tail Rotor
胡国才 1倪圆 2张学军 3徐吉辉4
作者信息
- 1. 海军航空工程学院飞行器工程系,山东烟台264001
- 2. 海军航空工程学院研究生管理大队,山东烟台264001
- 3. 海军装备部驻沈阳地区军事代表室,沈阳110034
- 4. 海军航空工程学院科研部,山东烟台264001
- 折叠
摘要
Abstract
Based on the ground icing-test data of a certain type of helicopter tail rotor, an analytical model of iced rotor aerodynamic performance was established. It was found that the lift and drag coefficients of NACA0012 blade section airfoil by the model correlated well with test data. Based on the established model, the characteristics of tail rotor blade airfoil was calculated both for clear and iced situations by Fluent code The results showed that icing reduced the lift coefficient and increased the drag coefficient of blade airfoil. At last, a method to analyzing aerodynamic characteristics of tail rotor on icing condition was formulated by using element -momentum theory in combination. The final results showed that icing could reduce the thrust coefficient and increase the torque coefficient, which significantly deteriorated the aerodynamic performance of the tail rotor.关键词
直升机/尾桨/桨叶结冰/气动性能Key words
helicopter/tail rotor/blade icing/aerodynamic performance引用本文复制引用
胡国才,倪圆,张学军,徐吉辉..桨叶结冰对尾桨气动性能的影响[J].海军航空工程学院学报,2011,26(4):365-369,5.
