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Brusov, V. (author), Grzybowski, J. (author), Petruchik, V. (author)
Flight investigations of aerodynamics and flight dynamics for micro-UAVs and mini-UAVs stimulate us to use automatic data acquisition systems to obtain valid estimations for UAV performances and characteristics. There exist many kinds of microprocessor-based and microcontroller-based data acquisition systems but all of them do not satisfy...
conference paper 2011
document
Brusov, V. (author), Petruchik, V. (author)
A reasonable selection of wing airfoil is very important part of aerodynamic design process for micro-UAVs. The selected airfoil predetermines substantially performances of the designed UAV. This reason causes us to pay attention to the problem of UAV wing airfoil selection taking into account properties specific for micro-UAVs. A concept of...
conference paper 2011
document
Thipyopas, C. (author), Intaratep, N. (author)
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...
conference paper 2011
document
Montazer Hojjat, H.R. (author)
In the design of Micro Aerial Vehicles, decreasing the size is one of the most common challenging aims and to approach this aim, the weight of the whole aircraft shall decrease and structure is the second part which has the most weight [13]. In this paper, the use of a shell structure made from Nylon 6/6 is studied. Nylon was chosen because of...
conference paper 2011
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