  In this paper I present the aerodynamic optimization of the angle of attack
of MQ-9 Reaper wings under turbulent airflow conditions. The background
discusses the evolution of UAVs such as the Hunter and their usages for
different tasks, specifically within the last decade. The main procedural stage
consists of creating a criterion for choosing the most aerodynamic wing design
by considering certain aerodynamic properties and analyzing the lift and drag
coefficients using computer software. At the end of the paper, the final
optimized MQ-9 wing design, along with its respective design parameters, are
presented and discussed.
