About this document

Morphing Effects on Airfoil Aerodynamics by Sameh Khalid is a document available to read on EtoBox.

This research article investigates the aerodynamic benefits of morphing airfoils, specifically focusing on combined droop nose and trailing-edge morphing. The study utilizes X-FOIL and ANSYS Fluent to optimize airfoil configurations, resulting in increased stall angles and improved lift-to-drag ratios. Key findings indicate that morphing can enhance aircraft maneuverability and reduce drag, with specific parameters yielding significant aerodynamic improvements compared to traditional airfoils.

Author

Sameh Khalid

Language

EN