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Micro Aerial Vehicle (MAV): An Aerodynamics Optimized Design

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Figure

FIGURE 1.1: Forces Acting on an Airplane
FIGURE 1.2: Coefficient of lift and drag with an aspect ratio of 5 [5]
Figure  2.2  shows  graph  of  Lift  Coefficient,  C L   versus  Angles  of  Attack,    of  rectangular plan form, with varying of aspect ratio
FIGURE 3.1: Methodology Flow Chart
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