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Airfoil Design for Flying Wing UAV by HARISH P is a document available to read on EtoBox.
What is Airfoil Design for Flying Wing UAV about?
The document summarizes research on designing an airfoil for a flying wing unmanned aerial vehicle (UAV). It describes using the XFOIL program to modify the Eppler E334 airfoil by increasing its thickness to chord ratio from 11.93% to 13.5%. Wind tunnel testing was used to verify the new airfoil design. The goal was to design an airfoil optimized for the flying wing configuration without a conventional fuselage or tail surfaces.
- Author
- HARISH P
- Language
- EN