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Home > Exam Questions > ATPL - Airline Transport Pilot Licence > Principles of Flight > For a thin, unswept aerofoil in classical linear theory, as the flow regime changes from subsonic to supersonic, the aerodynamic centre approximately:

255 - ATPL Question Bank in English - For a thin, unswept aerofoil in classical linear theory, as the flow regime changes from subsonic to supersonic, the aerodynamic centre approximately:

Question 255 - Principles of Flight - ATPL - Airline Transport Pilot Licence

Shifts aft by about 10%.

Remains unchanged.

Shifts from 25% to about 50% of the aerofoil chord.

Slightly shifts forward.

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