Experimental investigation of wing tip vortex

• المؤلفون الرئيسيون: Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali, Kwon, Kijung, Jung, Hyejin
• التنسيق: Conference or Workshop Item
• اللغة: English; English
• منشور في: 2009
• الموضوعات: TL500 Aeronautics
• الوصول للمادة أونلاين: http://irep.iium.edu.my/6029/1/Experimental_Investigation_of_Wing_Tip_Vortex.pdf; http://irep.iium.edu.my/6029/4/Experimental_investigation_of_wing_tip_vortex.pdf; http://irep.iium.edu.my/6029/; http://www.aiaa.org/agenda.cfm?lumeetingid=1811&viewcon=agenda&pageview=2&programSeeview=1&formatview=2

Particle image velocimetery was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a SWIM model was used as a vortex generator in two different configurations, (i) plain wing and (ii) flapped wing with trailing edge flap extended at 2...