Aerospace Engineering > GATE 2026 > Finite Wing Theory
An elliptic wing has a span of 6 m and a planform area of 6 m2. When generating a lift coefficient of 0.6, the induced drag it incurs is ________ × 10−3 (rounded off to 1 decimal place).

Correct : 114.6

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elliptic wing lift induced drag calculation GATE Aerospace Engineering 2026 aerospace engineering gate wing planform area lift coefficient 0.6 induced drag elliptic wing GATE 2026 Q35

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