Which of the following is NOT an advantage of a swept wing?

A swept wing design offers several aerodynamic advantages, particularly at higher speeds. One key benefit is the increased critical Mach number, which allows aircraft to cruise at higher speeds without encountering compressibility effects that can lead to a loss of lift. This higher cruising speed capability makes swept wings particularly effective for jet aircraft.

Another advantage of swept wings is reduced drag at those high speeds. By minimizing the cross-sectional area presented to oncoming airflow, swept wings can maintain better aerodynamic efficiency, allowing for a smoother airflow over the wing and less drag.

Dihedral stability, which helps with the aircraft's overall stability in flight, is also enhanced by swept wings. The wing's angle can contribute positively to roll stability, making it a suitable choice for various high-speed applications.

However, the statement regarding increased maximum lift is not accurate when comparing swept wings to straight wings. While swept wings can perform adequately and even effectively at higher speeds, they typically do not provide the same level of maximum lift at lower speeds as straight wings do. Straight wings are designed to generate more lift at lower airspeeds due to their larger surface area and higher aspect ratio, making them more effective for takeoff and landing scenarios. Thus, the claim about increased maximum lift associated with swept wings is not an