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Airfoil Shape Optimization for Improved Aerodynamics

Aeronautical and Aerospace Engineering
This 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.
openaire   +1 more source

Methods for Preliminary Airfoil Optimization

27th AIAA Applied Aerodynamics Conference, 2009
Ricardo Entz   +4 more
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Optimization of Flapping Airfoils for Maximum Thrust

41st Aerospace Sciences Meeting and Exhibit, 2003
Kaya, MUSTAFA, TUNCER, İSMAİL HAKKI
openaire   +2 more sources

Global optimization of multi-element airfoil

38th Structures, Structural Dynamics, and Materials Conference, 1997
Evin Cramer   +3 more
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Inverse airfoil design using design optimization

14th Applied Aerodynamics Conference, 1996
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