Poor wing fuselage will reduce lift loss.

Poor wing fuselage will reduce lift loss. Correct Answer False

A poorly designed fuselage can lead to drag rise, flow separation etc. As a result of these adverse effects lift loss will increase. Fuselage is considered as one of the primary drags producing member in an aircraft. Hence, an adequate design should be provided to reduce the lift loss.

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.