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For an F1 car, with a mass of 798kg and a desired downforce generated by the...

For an F1 car, with a mass of 798kg and a desired downforce generated by the rear wing which should equal to 3 times the weight of the car at the speed of 232km/h, if the lift coefficient of a chosen wing is 2.6 and the maximum wing span is limited to 1.5m, what would be the minimum chord length for the wing? Explain in this case whether or not this is a single element wing or multiple and why?

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