Aerospace Engineering > GATE 2015 > Aerodynamic Center and Center of Pressure
For constant free stream velocity and density, a change in lift for a large aspect ratio straight wing, with thin cambered airfoil section at small angles of attack, leads to
A
a shift of the aerodynamic center and no shift of the center of pressure
B
a shift of the center of pressure and no shift of the aerodynamic center
C
shift of both the aerodynamic center and the center of pressure
D
no shift either of the aerodynamic center or of the center of pressure

Correct : b

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Related Topics

aerodynamic center center of pressure lift change Aerospace Engineering GATE 2015 GATE AE 2015 Q17 large aspect ratio wing cambered airfoil aerodynamics

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