Number 2 in the drawing corresponds to the... See figure (PFA-010) (1,00 P.) Siehe Anlage 14
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Number 3 in the drawing corresponds to the... See figure (PFA-010) (1,00 P.) Siehe Anlage 14
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The angle of attack is the angle between...4
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The ratio of span and mean chord length is referred to as...4
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Which point on the aerofoil is represented by number 3? See figure (PFA-009) (1,00 P.) Siehe Anlage 24
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Which point on the aerofoil is represented by number 4? See figure (PFA-009) (1,00 P.) Siehe Anlage 24
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Wing tip vortex development begins during which phase of flight?4
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Which point on the aerofoil is represented by number 1? See figure (PFA-009) (1,00 P.) Siehe Anlage 24
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What pattern can be found at the stagnation point?4
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What pressure pattern can be observed at a lift-generating wing profile at positive angle of attack?4
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