Print Email Facebook Twitter Aerodynamics Study of Fixed-Wing MAV: Wind Tunnel and Flight Test Part of: International Micro Air Vehicle conference and competitions 2011 (IMAV 2011)· list the conference papers Title Aerodynamics Study of Fixed-Wing MAV: Wind Tunnel and Flight Test Author Thipyopas, C. Intaratep, N. Date 2011-09-12 Abstract Obtaining accurate aerodynamic characteristics of in-flight Micro Air Vehicles (MAVs) was viewed as difficult, due to the nature of very low Reynolds number, 3D complex flow, and strong influence from propulsion slipstream. This paper presents the study of the tailless, fixed-wing MAV, KuMAV-001, performed at Kasetsart University. The team investigated different analysis and testing methods to determine the aerodynamics characteristics of this MAV. The Vortex Lattice Method was introduced in the conceptual design phase and helped with the evaluation of the 3D effects for winglet configurations. The wind tunnel tests with main wing and fully configured MAV were conducted for powered and unpowered models. The influence of propulsion-induced flows on CL, CD, and CM(cg) was investigated during the wind tunnel testing. Verification of the performance results are to be completed with flight test data in the future. Subject Micro Air Vehicledesignaerodynamic properties To reference this document use: https://doi.org/10.4233/uuid:2d4b6f6d-d19d-4891-b965-225556e5bd57 Part of collection Conference proceedings Document type conference paper Rights (c) 2011 Thipyopas, C.; Intaratep, N. Files PDF IMAV2011SE_P15.pdf 1.47 MB Close viewer /islandora/object/uuid:2d4b6f6d-d19d-4891-b965-225556e5bd57/datastream/OBJ/view