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The pilot of an airplane executes a constant-speed loop-the-loop maneuver. His p

ID: 1413453 • Letter: T

Question

The pilot of an airplane executes a constant-speed loop-the-loop maneuver. His path is a vertical circle. The speed of the airplane is 285 mi/h, and the radius of the circle is 1450 ft.

(a) What is the pilot's apparent weight at the lowest point if his true weight is 160 lb? ______ lb

(b) What is his apparent weight at the highest point?__________ lb

(c) What If? Describe how the pilot could experience weightlessness if both the radius and the speed can be varied. (Note: His apparent weight is equal to the magnitude of the force exerted by the seat on his body.)

Explanation / Answer

Given,

v = 285 mi/hr = 418 ft/s ; R = 1450 ft ;

a) w = 160 lb => mg = 160 lb => m = 160/g = w/g

The pilots apparent weight at the bottom will be the sum of his actual weight and centripital force. So,

W = w + Fc = w + mv2/R = w + w/g (v2/R)

W = 160 + 160/32.2 ft/s^2 x 418 x 418 / 1450 = 758.75 lb

Hence, apparent weight = W = 758.75 lb

b)at the top, the apparent weight of the pilot will be, his weight minus centripital force on him. So,

W' = w - Fc = w - w/g (v2/R)

W' = 160 - 160/32.2 x 418 x 418 / 1450 = -438.75 lb

Hence, at the top, W' = -438.75 lb

c)The weigtlessness would be felt when,

Fc = w

w/g (v2/R) = w (w gets cancelled both the sides)

solving for R and v we get:

R = v2/g and v = sqrt (g R)

when, v = 418 ft/s R = 5426.21 ft and when, R = 1450 ft ; v = 216.07 ft/s

The radius and velocity required to attain weightlessness is independent of mass or weight of the pilot.

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