A military drone weighing 20N and having an equivalent surface area of 2m makes a flight...

 

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A military drone weighing 20N and having an equivalent surface area of 2m² makes a flight angle of 10° to the horizontal when flying in a wind of 20km/h, if the drive motor provides a force of 50N to maintain the drone position and this force of is inclined at 45° to the horizontal, calculate the lift and drag coefficients, assuming a density of air as 1.2kg/m³. A military drone weighing 20N and having an equivalent surface area of 2m² makes a flight angle of 10° to the horizontal when flying in a wind of 20km/h, if the drive motor provides a force of 50N to maintain the drone position and this force of is inclined at 45° to the horizontal, calculate the lift and drag coefficients, assuming a density of air as 1.2kg/m³.