Example: air traffic controller
Flight Thrust, Power, and Energy Relations
To obtain the required thrust or propulsive power via (9) or (10), we need the overall aircraft drag coefficient CD, which is broken down into three basic components. CD = CDA0 S + cd(CL,Re) + C2 L πAR (12) The first term gives the combined drag of all the non-wing components, such as the fuselage, tail, landing gear, etc.
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