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Analysis of Low Speed Aerodynamics of Double Delta Wing

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Figure

Figure 1: Schematic Diagram of Double-Delta wing  a) Top View b) Side View c) Bottom View
Table 3 shows the boundary conditions on the corresponding parts of the system under study
Figure 9: Flow at 20º angle of attack.
Figure 12 and Figure 13 shows the coefficient of pressure distribution with taping for 50% and 75% chord at 30º angle of attack respectively
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