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Design and Aerodynamic Analysis of Leading Edge For Morphing Wing by Jorge Luis Moreno Ortega is a document available to read on EtoBox.
This study presents the design and aerodynamic analysis of a morphing leading edge (MLE) for aircraft wings, focusing on optimizing aerodynamic efficiency through a drooping leading-edge mechanism. The research includes the evaluation of various configurations of a Watt-I six-bar mechanism and the optimization of stringer positioning to enhance load-carrying capacity during flight. Simulation results indicate significant improvements in aerodynamic performance compared to standard airfoils, with a prototype
- Author
- Jorge Luis Moreno Ortega
- Language
- EN