Normal force on the landing gear when the airplane lands

AI Thread Summary
To calculate the normal force on an airplane's landing gear during landing, the mass of the plane (25,000 kg) and landing speed (72 m/s) are essential. The normal force is influenced by the vertical displacement of the landing gear (0.92 m) and the angle of descent (5°). The calculations involve determining the change in kinetic energy and potential energy as the plane descends. The normal force is calculated to be approximately 664,750 N, factoring in both kinetic and potential energy losses. Understanding these dynamics is crucial for accurate force assessments during landing.
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Homework Statement


An airplane of mass 25,000 kg (approximately the size of a Boeing 737) is coming in for a landing at a speed of 72 m/s. Calculate the normal force on the landing gear when the airplane lands. Hint: You will use 0.92 m as the compression (vertical displacement) of the landing gear shock absorbers when the plane contacts the ground and 5° as the angle that the landing velocity makes with the horizontal.

Homework Equations




The Attempt at a Solution


plane N 9.8*25000=245000N
a=vf^2-vi^2/2*-.92=36.31m/s
Fn=245000=25000*36.31=664750N*******
dy=-.92
viy=-6.27
vfy=0
a=36.39


Not sure what I am doing wrong
 
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When the landing gear first touches the ground, what is the normal velocity? What is the normal kinetic energy? Can you somehow equate that energy with the work the force does as it travels over the 0.92m?
 
I thought that's why I did 0-6.7^2/2*9.2
44.89/1.8=24.93

sorry I had to I was mixing numbers from another question.
 
I can't figure out your numbers since you didn't define where they came from.

I should have added that in addition to the change in kinetic energy of the plane at the beginning and at the end of the 0.92m descent, there is also a loss of potential energy. Both are reduced by the action of the force over the given vertical distance.
 
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