한국항공운항학회지 (Journal of the Korean Society for Aviation and Aeronautics)
- 제14권4호
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- Pages.24-30
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- 2006
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- 1225-9705(pISSN)
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- 2466-1791(eISSN)
NACA 0012 에어포일의 경계층 거동이 근접 후류에 미치는 영향
Influence of Boundary Layer Behavior on the Near-Wake of an NACA 0012 Airfoil
- 발행 : 2006.12.31
초록
An experimental study was carried out in order to investigate the influence of boundary layer behavior on the near-wake at low Reynolds numbers. An X-type hot-film probe(55R51) was used to measure the near-wake of an NACA 0012 airfoil at static angles of attack
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