This paper presents the design, aerodynamic analysis, manufacturing, and energy feasibility assessment of DELICE 1A, a 5 m-wingspan solar-electric unmanned aerial vehicle (UAV) developed as a technology demonstrator toward high-altitude pseudo-satellite (HAPS) operation. The MO6070 airfoil is evaluated using XFLR5 batc...
S. Akgün, M. Acar, Y. Açar et al.· Journal of Physics, Conferen...· 0 citations
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