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Aerodynamic condensation evidences of supersonic expansion fans around a transonic F/A-18
Aerodynamic condensation evidences of supersonic expansion fans around a transonic F/A-18
Shock waves may appear as weak optical disturbances above airliners with supercritical wings
Shock waves may appear as weak optical disturbances above airliners with supercritical wings
NASA TF-8A in 1973
NASA TF-8A in 1973
Thomas McMurtry before his flight on the Vought F-8A Crusader Supercritical Wing Airplane
Thomas McMurtry before his flight on the Vought F-8A Crusader Supercritical Wing Airplane
Supercritical airfoil Mach number/pressure coefficient diagram (y axis: Mach number, or pressure coefficient, negative up; x axis: position along chor
Supercritical airfoil Mach number/pressure coefficient diagram (y axis: Mach number, or pressure coefficient, negative up; x axis: position along chord, leading edge left). The sudden increase in pressure coefficient at midchord is due to the shock.