Aerodynamic Investigation of Smart Flying Wing MAV
Aerodynamic Investigation of Smart Flying Wing MAV
Numerical simulations are performed to assess the feasibility of using embedded piezo sensors-actuators within thin wings to make them adaptive and therefore more aerodynamically efficient. If the method is found attractive and validated, could lead to design of practical smart MAV wings, but it also has more general application.
Document information
Aerodynamic Investigation of Smart Flying Wing MAV
2009
22 pages
Report
No indication
English
Aerodynamics , Aircraft , Computers, Control & Information Theory , Aerodynamic characteristics , Drones , Numerical analysis , Smart technology , Actuators , Piezoelectric materials , Thin wings , Mathematical models , Mav(Micro air vehicles) , Aerodynamic design and analysis , Piezoelectric sensors , Piezoelectric actuators , Numerical simulation
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