Question:
In thin airfoil theory the lift curve slope is usually considered as
In thin airfoil theory the lift curve slope is usually considered as
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Lift curve slope = change in lift coefficient with angle of attack.
Updated On: June 02, 2025
- \(0.10\) per degree
- \(0.11\) per degree
- \(0.09\) per degree
- \(2\pi\) radians
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The Correct Option is B
Solution and Explanation
Thin airfoil theory gives the lift curve slope as approximately \(2\pi\) per radian, which translates to about 0.11 per degree.
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