한국가시화정보학회:학술대회논문집
- 한국가시화정보학회 2001년도 Proceedings of 2001 Korea-Japan Joint Seminar on Particle Image Velocimetry
- /
- Pages.53-61
- /
- 2001
A PIV STUDY ON A DELTA WING(LEX) MODEL FLOW IN MODERN AIRCRAFT
- LEE Young-Ho (Korea Maritime University) ;
- SOHN Myoung-Hwan (Korea Air Force Academy) ;
- LEE Hyun (IIT Co.) ;
- KIM Jeong-Hwan (Graduate School, KMU) ;
- KIM Beom-Seok (Graduate School, KMU)
- 발행 : 2001.12.01
초록
Highly swept leading edge extensions(LEX) applied to delta wings have greatly improved the subsonic maneuverability of contemporary fighters. Fundamental approach by PIV method was adopted to study the basic flow of the vortex pair formation appearing on a delta wing model with or without LEX. Three angles of attacks
키워드