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Airfoil Shape Optimization for Improved Aerodynamics
Aeronautical and Aerospace EngineeringThis project focuses on the optimization of a custom airfoil by systematically analyzing the effects of camber percentage (2%– 6%), camber position (1– 6), and angle of attack (6°) while maintaining a fixed thickness of 12%. The primary objective is to maximize the lift- to-drag ratio (L/D) to enhance aerodynamic efficiency and stability.
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Methods for Preliminary Airfoil Optimization
27th AIAA Applied Aerodynamics Conference, 2009Ricardo Entz +4 more
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Optimization of Flapping Airfoils for Maximum Thrust
41st Aerospace Sciences Meeting and Exhibit, 2003Kaya, MUSTAFA, TUNCER, İSMAİL HAKKI
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Global optimization of multi-element airfoil
38th Structures, Structural Dynamics, and Materials Conference, 1997Evin Cramer +3 more
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Inverse airfoil design using design optimization
14th Applied Aerodynamics Conference, 1996openaire +1 more source
AIRFOIL OPTIMIZATION AND ANALYSIS WITH METAHEURISTICALGORITHM
ASLAN, SELÇUK +2 moreopenaire +1 more source

