The F-16 supersonic jet ‑ghter (Figure 3.37) with a mass 12,331 kg and a wing area of 27.8 m2 is cruising at an altitude of 40,000 ft at Mach number 2.1. The wing span is 9.45 m and the length of the fuselage is 15.3 m. Determine the wave drag of the aircraft, assuming the aircraft volume is 21.3 m2

The F-16 supersonic jet ‑ghter (Figure 3.37) with a mass 12,331 kg and a wing area of 27.8 m2 is cruising at an altitude of 40,000 ft at Mach number 2.1. The wing span is 9.45 m and the length of the fuselage is 15.3 m. Determine the wave drag of the aircraft, assuming the aircraft volume is 21.3 m2


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