南京航空航天大学学报（英文版）2026，Vol.43Issue(1)：15-26,12.DOI:10.16356/j.1005-1120.2026.01.002
基于转捩的雷诺数对翼型气动特性影响计算与实验研究
Research on Effects of Reynolds Number on Airfoil Flow Transition Position and Aerodynamic Characteristics by Calculation and Experiment
王菲 1张威 2陈笑天2
作者信息
- 1. 中国直升机设计研究所,景德镇 333000,中国||景德镇竹蜻蜓航空科技有限责任公司,景德镇 333000,中国
- 2. 中国直升机设计研究所,景德镇 333000,中国
- 折叠
摘要
Abstract
A flow transition prediction method for calculating effects of Reynolds numbers on aerodynamic characteristics of airfoil is developed,and the accuracy of the method is verified by wind tunnel experiment data and other calculation results.On these basics,the infrared thermal imager experiment results of the flow transition in low-speed wind tunnel and the aerodynamic characteristics experiment results with variable Reynolds number in high-speed wind tunnel are carried out respectively,and compared with the numerical results of helicopter rotor airfoil.Specially,effects of Reynolds numbers on airfoil aerodynamic characteristics by means of flow transition under different working conditions are researched and some meaningful conclusions are obtained.The calculation method,experiment method and results as well as the flow transition analysis conclusions for aerodynamic characteristics can be used for the design of helicopter rotor airfoil,especially for the helicopters under the high altitude and low Reynolds number working conditions.关键词
直升机旋翼翼型/雷诺数/转捩/气动特性Key words
helicopter rotor airfoil/Reynolds number/flow transition/aerodynamic characteristics分类
航空航天引用本文复制引用
王菲,张威,陈笑天..基于转捩的雷诺数对翼型气动特性影响计算与实验研究[J].南京航空航天大学学报（英文版）,2026,43(1):15-26,12.
