On its takeoff roll, the airplane starts from rest and accelerates according to a = ao - kv² where ao is the constant acceleration resultingfrom the engine thrust and -kv² is the acceleration due to aerodynamic drag. If að = 1.6 m/s², k = 0.000039 m ¹, and vis in meters persecond, determine the design length of runway required for the airplane to reach the takeoff speed of 271 km/h if the drag term is (a)excluded and (b) included.V0 = 0Answers:(a) Excluding drag, s= i(a) Including drag, S= iv=271 km/hm3

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On its takeoff roll, the airplane starts from rest and accelerates according to a = ao - kv² where ao is the constant acceleration resulting from the engine thrust and -kv² is the acceleration due to aerodynamic drag. If ao = 1.6 m/s², k = 0.000039 m ¹, and v is in meters per second, determine the design length of runway required for the airplane to reach the takeoff speed of 271 km/h if the drag term is (a) excluded and (b) included. Vo = 0 Answers: (a) Excluding drag, S= (a) Including drag, S= i v= 271 km/h m m

On its takeoff roll, the airplane starts from rest and accelerates according to a = ao - kv² where ao is the constant acceleration resulting from the engine thrust and -kv² is the acceleration due to aerodynamic drag. If ao = 1.6 m/s², k = 0.000039 m ¹, and v is in meters per second, determine the design length of runway required for the airplane to reach the takeoff speed of 271 km/h if the drag term is (a) excluded and (b) included. Vo = 0 Answers: (a) Excluding drag, S= (a) Including drag, S= i v= 271 km/h m m

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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