5.27 The airplane's weight is W = 2400 lb. Its brakes keep the rear wheels locked. The front (nose) wheel can turn freely, and so the ground exerts no horizontal force on it. The force T exerted by the airplane's propeller is horizontal. (a) Draw the free-body diagram of the airplane. Determine the reaction exerted on the nose wheel and the total normal reaction exerted on the rear wheels (b) when T = 0; (c) when T = 250 lb. T 4 ft W A-s ft B 2 ft' Problem 5.27
5.27 The airplane's weight is W = 2400 lb. Its brakes keep the rear wheels locked. The front (nose) wheel can turn freely, and so the ground exerts no horizontal force on it. The force T exerted by the airplane's propeller is horizontal. (a) Draw the free-body diagram of the airplane. Determine the reaction exerted on the nose wheel and the total normal reaction exerted on the rear wheels (b) when T = 0; (c) when T = 250 lb. T 4 ft W A-s ft B 2 ft' Problem 5.27
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![5.27 The airplane's weight is W = 2400 lb. Its brakes keep the
rear wheels locked. The front (nose) wheel can turn freely, and so
the ground exerts no horizontal force on it. The force T exerted by
the airplane's propeller is horizontal.
(a) Draw the free-body diagram of the airplane. Determine the
reaction exerted on the nose wheel and the total normal reaction
exerted on the rear wheels
(b) when T = 0;
(c) when T = 250 lb.
T
SNEMW
4 ft
W
A-s ft B
2 ft'
Problem 5.27](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fccddceb6-96d6-484c-8378-6d8620562c07%2F9a88ca51-11ce-4f20-a7e1-3adaa8ab1cce%2Fi4b6938_processed.jpeg&w=3840&q=75)
Transcribed Image Text:5.27 The airplane's weight is W = 2400 lb. Its brakes keep the
rear wheels locked. The front (nose) wheel can turn freely, and so
the ground exerts no horizontal force on it. The force T exerted by
the airplane's propeller is horizontal.
(a) Draw the free-body diagram of the airplane. Determine the
reaction exerted on the nose wheel and the total normal reaction
exerted on the rear wheels
(b) when T = 0;
(c) when T = 250 lb.
T
SNEMW
4 ft
W
A-s ft B
2 ft'
Problem 5.27
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