Nacelle for a bypass turbofan engine

A nacelle for a bypass turbofan engine comprising:

• an upstream section through which a flow of air penetrates, a middle section surrounding a fan of the turbofan engine, and a downstream section comprising an inner structure and an outer structure delimiting a tunnel through which the flow of air flows, the outer structure comprising at least one cowl mounted on the inner structure and movable along a longitudinal axis (Δ) of the nacelle so as to allow evacuation of at least part of the flow of air circulating in the tunnel during a thrust inversion phase of the nacelle, the nacelle also having a top receiving a fastening pylon for a wing of the aircraft, the nacelle comprising:
• at least one first panel mounted on the inner structure of one side of the nacelle, with respect to the top, that undergoes a more significant physical interference with an element of the wing than the other side of the nacelle, said panel being arranged to limit the physical interference of said cowl with said wing element during thrust reversal, and
• at least one second panel mounted on the other side of the nacelle, with respect to the top, said panel being arranged to increase the air discharged from the other side of the nacelle during thrust reversal.