How do tailless aircraft yaw? I was doing research on control surfaces present on an aircraft and I noticed that some aircraft like the B2 Spirit does not have a vertical tail stabilizer and therefore no rudder either.

How do aircraft such as these perform turns and counteract adverse yaw in banked curves? Do they apply some sort of differential thrust system for turning?
Technically the B-2 bomber has rudders, they are &quot;drag rudders&quot; (or split rudder) and are located on the outer portion of the wing:

Source: Quora
The rudders open in a clamshell configuration to create a drag force on the outer part of the wing. Because these are on the outer part of the wing, they can create a significant yaw force.