At same value of maximum lift AOA, lift coefficient of Cambered wing is _________

At same value of maximum lift AOA, lift coefficient of Cambered wing is _________ Correct Answer higher than uncambered wing

Lift coefficient at maximum lift AOA for a cambered wing is higher than that of the uncambered wing. At maximum lift AOA, value of lift coefficient will be maximum as well. Further increase in angle will reduce the amount of lift generated by wing.

Related Questions

A subsonic aircraft has unswept wing which has maximum lift coefficient of 1.4. Now, consider wing is provided sweep of 25° at quarter chord point. Now, determine the change in maximum lift coefficient due to the provision of sweep.