Browse by Subject "XFOIL"
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(2012-05-22)Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with trailing edge plain flaps in an attempt to understand the effects of Reynolds number, percent thickness (t/c), percent chord of ...
(2015-12-11)This thesis presents a process to optimize a cambered airfoil with the MATLAB genetic algorithm (GA) and a multipoint inverse method called PROFOIL. XFOIL was used to evaluate the aerodynamic performance of each airfoil. ...