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For questions about those devices that swing forwards and downwards from the leading edge of an aircraft's wings, allowing them to produce more lift without stalling. Questions about high-lift devices in general should use "high-lift-devices" instead.

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Is it pragmatic to use slats and flaps to maintain position of center of lift?

to this with an amateur understanding of CL, Cp and their contribution to the overall lift of a wing, so bear with me :) I have been wondering for some time about whether you could design a system of slats
Timothy Cater's user avatar