The patterns of air pressure that create lift and drag at supersonic speeds are dramatically different from those that create lift and drag at subsonic speeds.
When an aircraft approaches the speed of sound, the airflow
over the wing reaches supersonic speed before the airplane itself
does, and a shock wave forms on the wing. The airflow behind the
shock wave breaks up into a turbulent wake, which increases drag.
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When the airplane exceeds the speed of sound, a shock wave
forms just ahead of the wing's leading edge. The shock wave that
formed on the wing is now at the trailing edge.
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When the wing is tilted upward, a shock wave forms below its
leading edge, and an expansion wave (or sometimes a weaker shock
wave) forms above its leading edge. The higher pressure behind
the shock wave and lower pressure behind the expansion wave
result in a single force that pushes the wing both upward and
backward. The upward part of this force is lift; the backward
part of this force is drag.
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(Rev. 02/16/99)