Aerodynamics investigation of MAV with flexible wing

• المؤلف الرئيسي: Zeng, Zibin
• مؤلفون آخرون: Go Tiauw Hiong
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2011
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aerodynamics
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/44674

This report describes research performed on various configurations of a flexible-wing Micro Air Vehicle (MAV). Flexible-wing MAV’s advantage over rigid-wing MAV is that it is able to fly much smoother in gusty wind conditions. As such, wind tunnel experiments at free stream velocity of 21 m/s were c...