An aircraft loops the loop of radius R = 500 m with a constant velocity v = 360 km/hour. The weight of the flyer of mass m = 70 kg in the lower, upper and middle points of the loop will respectively be- (a) 210 N, 700 N, 1400 N (b) 1400 N, 700 N, 2100 N (c) 700 N, 1400 N, 210 N (d) 2100 N, 700 N, 1400 N
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a is great answer
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