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Design and Analysis of Wing of an Ultralight Aircraft

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Figure

Fig. 1. An ultralight aircraft
Fig. 2. Images from CATIA (a) Sketch of the airfoil (b) Rib sections with spar (c) Wing section with skin
Fig. (a) shows mesh with No. of nodes= 221821 & No. of elements= 1251417, (b) mesh with No
Fig. 4. Total pressure (a) on the bottom portion of wing (b) on the top portion of the wing
+7

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