Fig. 19From: A low-boom and low-drag design method for supersonic aircraft and its applications on airfoilsThe ground boom signatures and drag coefficients for the baseline and optimized NACA0008 airfoil with different angles of attack. a the maximum overpressure vs the angle of attack; b the maximum underpressure vs the angle of attack; c comparison of the ground boom signature at the angle of attack = 3o; d the drag coefficient vs the angle of attack; e the lift coefficient vs the angle of attack; f the lift-drag ratio vs the angle of attackBack to article page