The Cessna 172 Skyhawk aircraft is a four-seat, single-engine airplane produced by the Cessna Aircraft Company. Over 43,500 Cessna 172s have been built, making it the most common aircraft. The basic design of the Cessna 172 uses the NACA 2412 Aerofoil in a high wing configuration. The chord length of the wing for the Cessna 172R (Skyhawk) is 1.63 meters (5 ft 4 in) at the wing root, and 1.12 meters (3 ft 8 in) at the wing tip. Therefore, the calculated average chord length is 1.472 meters (4.83 ft). It has a cruise speed of 124 knots 75% power at 8,000 feet. At 8,000 feet Calculate the lift at cruise speed Calculate the Drag at cruise speed Calculate the L/D ratio at cruise speed What is the stall angle for this aircraft? woment coefficient Section lift coefficient, c 2.0 1.6 -12 -1.6 U -16 Section anale of attack, ded Dimensions.Guide | Cessna 172 Skyhawk 10 112" 3.4 m 311 12m 8'11" 2.72 m -36 111 m 2,54 m 272 8.28 m