Skip to main content
Fig. 19 | Advances in Aerodynamics

Fig. 19

From: A low-boom and low-drag design method for supersonic aircraft and its applications on airfoils

Fig. 19

The 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 attack

Back to article page