The drag equation of an aircraft is given by the equation: Cp = 0.03 + 0.02 C The weight of the aircraft is 100 kN. What is the value of drag when flying straight, level and unaccelerated under minimum drag conditions? %3D

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The drag equation of an aircraft is given by the equation:
Cp = 0.03 +0.02 C}
The weight of the aircraft is 100 kN. What is the value of drag when flying
straight, level and unaccelerated under minimum drag conditions?
Transcribed Image Text:The drag equation of an aircraft is given by the equation: Cp = 0.03 +0.02 C} The weight of the aircraft is 100 kN. What is the value of drag when flying straight, level and unaccelerated under minimum drag conditions?
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