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.
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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)