Question: 7. Given: A fixed-wing aircraft with total parasite drag equal to 800 lbs. The aircraft is flying at 20,000 ft. STP, at 300 KTAS.

7. Given: A fixed-wing aircraft with total parasite drag equal to 800

7. Given: A fixed-wing aircraft with total parasite drag equal to 800 lbs. The aircraft is flying at 20,000 ft. STP, at 300 KTAS. What is the correct f(equivalent drag area) and C (coefficient of parasite drag) if the wing area is 400 ft? CDP Dp

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