Fig. 21From: A low-boom and low-drag design method for supersonic aircraft and its applications on airfoilsThe comparison of ground boom signatures a for the diamond airfoil baseline and the optimized diamond airfoil at the mass flow rate = 6.5 kg/s b for the NACA0008 airfoil baseline and the optimized NACA0008 airfoil at the mass flow rate = 7.5 kg/sBack to article page