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A jet transport with a landing speed of 200 km/hr reduces its speed to 60 km/hr with a negative thrust R from its jet thrust reversers in a distance of 410 m along the runway with constant deceleration. The total mass of the aircraft is 135 Mg with mass center at G. Compute the reaction N under the nose wheel B toward the end of the braking interval and prior to the application of mechanical braking. At the lower speed, aerodynamic forces on the aircraft are small and may be neglected. G 2.6 m B 14 m. R 1.6 m A -2.5 m N = 0 kN

A jet transport with a landing speed of 200 km/hr reduces its speed to 60 km/hr with a negative thrust R from its jet thrust reversers in a distance of 410 m along the runway with constant deceleration. The total mass of the aircraft is 135 Mg with mass center at G. Compute the reaction N under the nose wheel B toward the end of the braking interval and prior to the application of mechanical braking. At the lower speed, aerodynamic forces on the aircraft are small and may be neglected. G 2.6 m B 14 m. R 1.6 m A -2.5 m N = 0 kN

Traffic and Highway Engineering
Traffic and Highway Engineering
5th Edition
ISBN:9781305156241
Author:Garber, Nicholas J.
Publisher:Garber, Nicholas J.
Chapter3: Characteristics Of The Driver, The Pedestrian, The Bicyclist, The Vehicle, and The Road
Section: Chapter Questions
Problem 10P
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A jet transport with a landing speed of 200 km/hr reduces its speed to 60 km/hr with a negative thrust R from its jet thrust reversers in a distance of 410 m along the runway with constant deceleration. The total mass of the aircraft is 135 Mg with mass center at G. Compute the reaction N under the nose wheel B toward the end of the braking interval and prior to the application of mechanical braking. At the lower speed, aerodynamic forces on the aircraft are small and may be neglected. G 2.6 m B 14 m. R 1.6 m A -2.5 m N = 0 kN
Transcribed Image Text:A jet transport with a landing speed of 200 km/hr reduces its speed to 60 km/hr with a negative thrust R from its jet thrust reversers in a distance of 410 m along the runway with constant deceleration. The total mass of the aircraft is 135 Mg with mass center at G. Compute the reaction N under the nose wheel B toward the end of the braking interval and prior to the application of mechanical braking. At the lower speed, aerodynamic forces on the aircraft are small and may be neglected. G 2.6 m B 14 m. R 1.6 m A -2.5 m N = 0 kN
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