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Basics, laws and definitions
The two-dimensional airflow about an aerofoil
The coefficients
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The total drag
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The relation between the lift coefficient and the speed for constant lift
The stall
CLmax augmentation
Means to decrease the CL - CD ratio, increasing drag
The boundary layer
Special circumstances
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When pulling out of a dive (e.g. looping) the angle of attack:
increases.
decreases.
remains the same.
cannot be increased at all for structural reasons.
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