What can cause a loss of lift inboard on a swept wing during flight?

The phenomenon of a loss of lift inboard on a swept wing during flight can be attributed to the shock wave effect at the thick root of the wing. In swept-wing designs, the airflow over the wing can become supersonic at high speeds, particularly near the thicker section of the wing (the root). When the airflow transitions to supersonic, shock waves form, altering the distribution of pressure over the wing's surface. This change in pressure can lead to a significant reduction in lift, especially inboard where the wing thickness is greatest. This effect is critical for pilots and aircraft designers to understand, particularly when operating at high speeds where shock wave formation becomes a factor.

The other options presented do not address this specific aerodynamic issue related to swept wings effectively. While a reduction in engine thrust or increased wing loading can influence overall lift, they do not specifically highlight the unique characteristics of shock waves in the context of a swept-wing design. Favorable wind conditions might provide benefits for flight performance, but they do not directly cause a loss of lift.