Dynamics - Airplane stopping on a runway

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    Airplane Dynamics
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An airplane with a mass of 5Mg and a touchdown speed of 300 m/hr requires calculations to determine the distance needed to reduce its speed to 150 km/hr after deploying a braking parachute. The drag force is modeled as D = k*(v^2), with 'k' calculated as 120,000 Newtons/(83 m/s)^2. The discussion focuses on applying Newton's second law to derive acceleration and subsequently integrating to find displacement. Participants express confusion about how to proceed with the integration due to the dependence of acceleration on velocity. The calculated distance to stop, as per the textbook, is 201 meters, but users seek clarification on the integration process.
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Homework Statement


an airplane has a mass of 5Mg has a touchdown speed of 300m/hr. At which instant the braking parachute is deployed and the power shut off. If the total drag on the aircraft varies with velocity as shown in the accompanying graph, calculate the distance x along the runway required to reduce the speed to 150km/hr. Aproximate the variation of the drag by an equation D=k*(v^2). where 'k' is a constant.



Homework Equations


integral of (vdv)=a* integrate ds



The Attempt at a Solution


The constant 'k' was found to be 120,000 Newtons/(83m/s)^2
from the graph. Then, how to calculate the displacement is where the help is needed. The calculated answer from the back of the of the book is 201m. Any help on this problem would be appreciated.
thanks


 

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I see no "attempt at a solution". Are you not even trying?
 
auburntigers_dy,

I don't think that the "relevant equation" you cited is all that relevant. Can you write down Newton's second law for this problem? That would be a good start.
 
tom mattson,
Newton's second law is f=m*a. ma=kv^2. therefore a=(kv^2)/m. This is where the relevant equation that i cited could be used, where the acceleration is calculated and velocity is given which then leaves you with the unknown term delta x. I am stuck on what velocity would i use to solve for this delta x.
 
dynamics

HallsofIvy said:
I see no "attempt at a solution". Are you not even trying?


Hallsofivy,

i solved for k, the drag force is kv^2 which i equated it to Newton's second law Mass*acceleration. Then solving for acceleration resulted in k*v^2/(5000kg). then I integrated the relevant the relevant equation vdv=ads to solve for ds. The confusion lies in the calculated acceleration which is also expressed in terms of velocity which leaves stuck upon how to solve for displacement.
 
dynamics

HallsofIvy said:
I see no "attempt at a solution". Are you not even trying?


Hallsofivy,

i solved for k, the drag force is kv^2 which i equated it to Newton's second law Mass*acceleration. Then solving for acceleration resulted in k*v^2/(5000kg). then I integrated the relevant equation vdv=ads to solve for ds. The confusion lies in the calculated acceleration which is also expressed in terms of velocity which leaves me stuck upon how to solve for displacement. everything is expressed in terms of velocity.
 
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