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