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Home > Exam Questions > ATPL - Airline Transport Pilot Licence > Principles of Flight > In classical thin-aerofoil theory for an unswept symmetrical aerofoil producing lift in supersonic flow, the centre of pressure is approximately:

291 - ATPL Question Bank in English - In classical thin-aerofoil theory for an unswept symmetrical aerofoil producing lift in supersonic flow, the centre of pressure is approximately:

Question 291 - Principles of Flight - ATPL - Airline Transport Pilot Licence

Near the leading edge.

At the quarter-chord position (about 25% chord).

Near the trailing edge.

At the mid-chord position (about 50% chord).

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