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Airfoil Testing to Obtain Full-range Aerodynamic Characteristics based on Velocity Field Measurements Utilizing a Digital Wind Tunnel

익형의 전 범위 받음각에서 공력특성 시험이 가능한 디지털 풍동의 개발 및 속도장 측정

  • Kang, Sangkyun (Department of Mechanical Engineering, Kunsan National University) ;
  • Kim, Jin-Ok (Department of Mechanical Engineering, Kunsan National University) ;
  • Kim, Yong-Su (Department of Mechanical Engineering, Kunsan National University) ;
  • Shin, Won-Sik (Power Service Wind Turbine O&M Team, Doosan Enerbility) ;
  • Lee, Sang-Il (Offshore Wind Energy Institute, Kunsan National University) ;
  • Lee, Jang-Ho (School of Mechanical System Engineering, Kunsan National University)
  • Received : 2022.02.21
  • Accepted : 2022.06.28
  • Published : 2022.09.25

Abstract

A wind tunnel provides artificial airflow around a model throughout the test section for investigating aerodynamic loads. It has various applications, which include demonstration of aerodynamic loads in the building, automobile, wind energy, and aircraft industries. However, owing to the high equipment costs and space-requirements of wind tunnels, it is challenging for numerous studies to utilize a wind tunnel. Therefore, a digital wind tunnel can be utilized as an alternative for experimental research because it occupies a significantly smaller space and is easily operable. In this study, we performed airfoil testing based on velocity field measurements utilizing a digital wind tunnel. This wind tunnel can potentially be utilized to test the full-range aerodynamic characteristics of airfoils.

Keywords

Acknowledgement

This work was supported by Korea Institute of Energy Technology Evaluation and Planning (KETEP) grant funded by the Korea government (MOTIE) (20213030020380, Development of adhesive -type modular blades over 70m for overcoming onshore transportation limitation) and by the Ministry of Education(NRF-2017R1D1A3B06032145).

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