Aerodynamic characterization of certain wing sections utilizing computational fluid dynamics techniques
M.Ing. === The aim of this dissertation is to apply numerical aerodynamic principles to the characterization of an alternative stepped aerofoil concept. The accurate and efficient determination of the aerodynamic forces caused by the relative fluid motion and the consequent lift and drag coefficient...
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2012
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| Online Access: | http://hdl.handle.net/10210/6433 |