Publications

Comparative study of wing lift distribution analysis for high altitude long endurance (HALE) unmaned aerial vehicle

Published in Journal of Physics: Conference Series (JPCS), 2018

Preliminary analysis of HALE UAV lift distribution of the wing presented to give decisive consideration for its early development. Theoretical approach using non-linear lifting line theory will be compared with modern numerical approach using Computational Fluid Dynamics (CFD). The results of wing lift distribution calculated from both methods will be compared to study the reliability. Read more