72. The aircraft mass m = 3T for takeoff must have a sp

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72. The aircraft mass m = 3T for takeoff must have a speed V = 360 km / h and the length of the run-up S = 600m. What should be the minimum engine power Nmin, required for take-off the plane? Resistance force considered proportional to the force of normal pressure, the average drag coefficient taken equal to f = 0,2. The movement of aircraft during acceleration occurs uniformly accelerated.

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Detailed solution. Decorated in Microsoft Word 2003. (Target decided to use formula editor)


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