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.

• A. Maximum Lift coefficient will be reduced by 0.2580 amount
• B. Increment by 1.245
• C. Decreases by 0.0476 amount
• D. Maximum lift coefficient will increase by 56%