The angle of attack (aerodynamic angle of incidence) of an aerofoil is the angle between the:4
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The units of wing loading (I) W / S and (II) dynamic pressure q are:4
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The angle between the aeroplane longitudinal axis and the chord line is the:4
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On a symmetrical aerofoil, the pitching moment for which CL = 0 is:4
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Dihedral of the wing is:4
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If the continuity equation is applicable, what will happen to the air density (rho) if the cross sectional area of a tube changes? (low speed, subsonic and incompressible flow)4
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Which of the following wing planforms produces the lowest induced drag? (all other relevant factors constant)4
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The induced drag coefficient, CDi is proportional to:4
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If an aeroplane flies in the ground effect4
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Which statement is correct about the laminar and turbulent boundary layer:4
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