The airfoil chord length c = 2.8 m. The max. thickness is t= 0.03. Find the maximum thickness in millimeters. Answer:
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The airfoil chord length c = 2.8 m. The max. thickness is t= 0.03. Find the maximum thickness in millimeters. Answer:
The airfoil chord length c = 2.8 m. The max. thickness is t= 0.03. Find the maximum thickness in millimeters. Answer:
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