The tailplane usually becomes more effective as a stabiliser at high Mach numbers because there are decreases of wing lift-curve slope and rate of change of downwash with mean lift coefficient. The latter effect is mainly due to the wing-root shock stalling at a lower Mach number than the rest of the wing.

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shock stalls

（ present singular third-person ）

shock stalling

（ participle present ）

shock stalled

（ participle past ）

shock stalled

（ past ）

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shock stall

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shock stall

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