draveon556 draveon556 27-02-2024 Physics contestada An aircraft with a drag coefficient of 0.95 and a frontal area of 10m² is traveling at a Mach number of 0.7 in air with a static pressure of 101 kPa. Calculate the drag produced by this aircraft. a. 665 N b. 6650 N c. 950 N d. 9500 N