Print Email Facebook Twitter Design Approach for Selection of Wing Airfoil with Regard to Micro-UAVs Part of: International Micro Air Vehicle conference and competitions 2011 (IMAV 2011)· list the conference papers Title Design Approach for Selection of Wing Airfoil with Regard to Micro-UAVs Author Brusov, V. Petruchik, V. Date 2011-09-12 Abstract 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 multitask design is suggested to solve this kind of problems. This concept is explained in regard to selection process for micro-UAV airfoil. Presented simulation results demonstrate that using of multitask approach to aerodynamic design of micro-UAV enables us to enhance UAV efficiency due to improvement of its aerodynamic perfection. Subject Micro Air Vehicledesignairfoil To reference this document use: https://doi.org/10.4233/uuid:2b261a19-fae4-44dd-ac04-1113ebc7c89b Part of collection Conference proceedings Document type conference paper Rights (c) 2011 Brusov, V.; Petruchik, V. Files PDF IMAV2011SE_P19.pdf 571.09 KB Close viewer /islandora/object/uuid:2b261a19-fae4-44dd-ac04-1113ebc7c89b/datastream/OBJ/view