Guest625101138
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Oops. we cross posted.
Actually, I'm not familiar with those abbreviations. But that's ok.
Since the plane is taking off with a 3 m/s tailwind, the indicated airspeed would be 7 m/s.
The derating comes in from the need to accelerate to a higher kinetic energy before taking off. In other words, if we say that the plane can lift off at 10m/s, we have a certain amount of kinetic energy. But with the tailwind, we now have to accelerate to 13 m/s with a correspondingly higher KE. The power needed to spin the wheels has increased too since they are now traveling faster across the ground. The engine can only supply the KE so fast (limited by its horsepower), so it takes longer to get off the ground.
All I would like to know in the case with the airplane is what does the propeller thrust of 2000N reduce to because it is acting on an airstream and likewise what does the 1000N become because it is being applied by an airstream. Show how you use the KE and horsepower to derate the forces.
I have no pilot training so I am interested in how pilots calculate derating factors for forces acting on, or applied by, an airstream. You did it for my buggy model but I am having trouble applying the same principle to an airplane. I understand this is an area where pilots have a lot of training and knowledge.