Question: Consider the BD - 5 J . Wing span: 1 7 , Wing planform area 3 7 . 8 2 , Gross weight at takeoff:

Consider the BD-5J. Wing span: 17, Wing planform area 37.82, Gross weight at takeoff: 962, Power plant: OneFrench-built Microturbo TRS 18 turbojet engine with maximum thrust at sea level of 202. We will approximate the drag polar for this airplane by CD =0.022+0.064()2 estimate the Absolute ceiling.NOTE. USE INTERVALS OF 1000
()

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