Open AccessExperimental Study on High Speed Two-dimensional Airfoil Based on Conventional High Speed Wind Tunnel Test
Author(s) -
Yi Wang,
Tao Zhou
Publication year - 2020
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1626/1/012183
Subject(s) - airfoil , wind tunnel , hypersonic wind tunnel , wind speed , supersonic wind tunnel , reynolds number , subsonic and transonic wind tunnel , wind gradient , marine engineering , relative wind , structural engineering , engineering , wind direction , aerodynamics , meteorology , aerospace engineering , angle of attack , physics , transonic , turbulence
The wind tunnel test of two-dimensional airfoil is usually carried out in the special wind tunnel for the airfoil test, but this kind of wind tunnel is usually small in size and low in Reynolds number. On the contrary, the conventional wind tunnel test is generally large in size, in which higher test Reynolds number can be obtained, but there is wall interference and other problems to overcome at the same time. In this study, the RAE2822 airfoil was used to carry out the wind tunnel test of high-speed two-dimensional airfoil in FL-3, which is a large-scale conventional high-speed wind tunnel and the section pressure coefficient was measured. Experimental data after calculation and correction comparing with the standard model data shows that it is practically possible to carry out airfoil wind tunnel test in conventional high-speed wind tunnel.