Fig. 9From: 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 diamond airfoil with different mass flow rates. a the maximum overpressure vs the mass flow rate; b the maximum underpressure vs the mass flow rate; c the drag coefficient vs the mass flow rate; d the lift coefficient vs the mass flow rate; e the lift-drag ratio vs the mass flow rateBack to article page