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Home > Exam Questions > ATPL - Airline Transport Pilot license > Principles of Flight > In the transonic range lift will decrease at the shock stall due to the

379 - ATPL - In the transonic range lift will decrease at the shock stall due to the

Question 379 - Principles of Flight - ATPL - Airline Transport Pilot license

Attachment of the shock wave on the trailing edge of the wing.

First appearance of a shock wave at the upper side of the wing.

Separation of the boundary layer at the shock waves.

Appearance of the bow wave.

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