For a laminar boundary
layer (BL) at an angle of attack (AOA) well below the stall AOA:

Question

Answer

the friction drag is
larger compared to the case of turbulent BL

Answer

if any, the flow
detachment point is usually closer to the TE compared to the case of turbulent
BL

Answer

the BL
is always laminar at the beginning

Answer

if existing, the wake or
pressure drag is smaller compared to the case of turbulent BL

Answer

none of the other options is correct

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