How far does an airliner wheel slip before rolling without slipping?

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Homework Help Overview

The problem involves calculating the distance an airliner's wheel slips on the runway before it begins to roll without slipping. It includes parameters such as the wheel's radius, mass, normal force, airliner speed, and the coefficient of sliding friction.

Discussion Character

  • Exploratory, Assumption checking

Approaches and Questions Raised

  • The original poster attempts to derive the distance slipped using torque and kinematic equations but arrives at a different answer than expected. Some participants question the interpretation of the displacement calculated, suggesting a misunderstanding between the wheel's tangential distance and the airliner's overall movement.

Discussion Status

The discussion is ongoing, with participants clarifying concepts related to angular displacement and its relation to the airliner's motion. There is an acknowledgment of a potential misunderstanding, but no consensus has been reached yet.

Contextual Notes

Participants are working under time constraints due to an upcoming test, which may influence the urgency of the discussion.

bowma166
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Homework Statement


When the wheels of a landing airliner tough the runway, they are not rotating initially. The wheels first slide on the runway (and produc eclouds of smoke and burn marks on the runway, which you may have noticed), until the sliding friction force has accelerated the wheels to the rotational speed required for rolling without slipping. From the following data, calculate how far the wheel of an airliner slips before it begins to roll without slipping: the wheel has a radius of 0.60 m and a mass of 160 kg, the normal force acting on the wheel is 2.0 x 105 N, the speed of the airliner is 200 km/h, and the coefficient of sliding friction for the wheel on the runway is 0.80. Treat the wheel as a uniform disk.

Homework Equations


\vec{\tau}=\vec{F}\times\vec{R}

|\tau|=I\alpha

F_{friction}=\mu_{k}N

I_{disk}=\frac{1}{2}MR^{2}

a=\alpha R

v^{2}=v_{0}^{2}+2ax

The Attempt at a Solution


Basically, it's a wheel with a force applied at one point that creates a torque up to a certain acceleration. So... I started with \tau=RF=I\alpha, substituted in for I, alpha, and F, and solved for a:
R\mu_{k}N=\left(\frac{1}{2}MR^{2}\right)\left(\frac{a}{R}\right)

\mu_{k}N=\frac{1}{2}Ma

\frac{2\mu_{k}N}{M}=a

I then substituted that value of a into the v2=whatever kinematics equation:

v^{2}=v_{0}^{2}+2\left(\frac{2\mu_{k}N}{M}\right)x

x=\frac{Mv^{2}}{4\mu_{k}N}

Plugging in the given values, I get x = .772 m. The book says that the answer is 1.6 m. What am I doing wrong? It is kind of weird that they give you R but I didn't have to use it.

Thanks.
 
Last edited:
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Anyone have any ideas? (Sorry for bumping so early like this but I need to sleep soon and I've got a test tomorrow. Heh.)
 
You're confusing angular displacement of a point on the wheel and the displacement of the airliner. The 'x' you solved for, therefore, is the tangential distance traveled by a point on the wheel, nothing to do with how far the airliner itself moves.
 
Oh, whoops. Thanks.
 

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