Aerospace Engineering > GATE 2021 > Induced Drag
A finite wing of elliptic planform with aspect ratio 10, whose section is a symmetric airfoil, is placed in a uniform flow at 5 degrees angle of attack. The induced drag coefficient for the wing is _______. (round off to three decimal places)

Correct : 0.005 to 0.009

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induced drag coefficient elliptic planform wing aspect ratio 10 uniform flow angle of attack aerospace engineering GATE 2021 drag coefficient calculation induced drag GATE aerospace engineering 2021

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