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Home > Exam Questions > ATPL - Airline Transport Pilot Licence > Principles of Flight > For a conventional aerofoil at positive lift, assume its first local supersonic region forms on the upper surface. Just above the critical Mach number, the first compression shock at the downstream boundary of that region appears on the:

289 - ATPL Question Bank in English - For a conventional aerofoil at positive lift, assume its first local supersonic region forms on the upper surface. Just above the critical Mach number, the first compression shock at the downstream boundary of that region appears on the:

Question 289 - Principles of Flight - ATPL - Airline Transport Pilot Licence

Leading edge of the wing.

Lower side of the wing.

Trailing edge of the wing.

Upper side of the wing.

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