Calculate the deceleration of an aircraft during landing rollout given the following conditions: Ta (average) = 575

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Calculate the deceleration of an aircraft during landing rollout given the following conditions:

Ta (average) = 575 lb Average drag = 1300 lb Average braking/rolling friction = 4200 lb Aircraft weight = 12 000 lb Assumptions = Constant deceleration, standard day, sea level conditions.

a. 10.2 fps

b. 16.3 fps

c. 11.3 fps

d. 13.2 fps

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Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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