Wind tunnel test of a ducted fan micro air vehicle during hover flight

• المؤلف الرئيسي: Tan, Yi Xiang.
• مؤلفون آخرون: Go Tiauw Hiong
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2010
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aerodynamics
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/39537
• المؤسسة: Nanyang Technological University

This study was focused on a ducted fan micro air vehicle (MAV) that combines the exceptional hover capabilities of rotary wing aircraft with the endurance and speed performance of fixed wing aircraft. The purpose of this research was to evaluate the aerodynamic performance of the ducted fan MAV duri...