2/39 On its takeoff roll, the airplane starts from rest and accelerates according to a = ao-ku², where a, is the con- stant acceleration resulting from the engine thrust and -ku² is the acceleration due to aerodynamic drag. If ao = 2 m/s², k = 0.00004 m¹, and vis in meters per sec- ond, determine the design length of runway required for the airplane to reach the takeoff speed of 250 km/h if the drag term is (a) excluded and (b) included. Vo = 0 v = 250 km/h

2/39 On its takeoff roll, the airplane starts from rest and accelerates according to a = ao-ku², where a, is the con- stant acceleration resulting from the engine thrust and -ku² is the acceleration due to aerodynamic drag. If ao = 2 m/s², k = 0.00004 m¹, and vis in meters per sec- ond, determine the design length of runway required for the airplane to reach the takeoff speed of 250 km/h if the drag term is (a) excluded and (b) included. Vo = 0 v = 250 km/h

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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Question

2/39 On its takeoff roll, the airplane starts from rest and
accelerates according to a = ao - ku², where ao is the con-
stant acceleration resulting from the engine thrust and
-ku² is the acceleration due to aerodynamic drag. If
ao = 2 m/s², k = 0.00004 m-¹, and vis in meters per sec-
ond, determine the design length of runway required for
the airplane to reach the takeoff speed of 250 km/h if the
drag term is (a) excluded and (b) included. lend loodw
Vo = 0
di nidristab
v = 250 km/h
redw
berm
1917
oda ajoaqui
PROBLEM 2/39qa to Income erit

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