Circular motion - plane going around a loop

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SUMMARY

A pilot flying an airplane in a vertical circular loop at a constant speed of 160 m/s experiences an apparent weight at the top of the loop that is one-third of his true weight. The correct radius of the circular path is calculated to be 1960 m. The initial calculation yielded an incorrect radius of approximately 3918.37 m due to a misunderstanding of the normal force's direction when the pilot is upside down. The normal force acts in the same direction as the weight at the top of the loop, providing the necessary centripetal acceleration.

PREREQUISITES
  • Understanding of Newton's second law (F_net = ma)
  • Knowledge of centripetal acceleration (a_normal = v^2 / R)
  • Familiarity with forces acting on objects in circular motion
  • Basic principles of weight and normal force in physics
NEXT STEPS
  • Study the concept of centripetal force in circular motion
  • Learn about the effects of acceleration on apparent weight
  • Explore the role of normal force in different orientations
  • Investigate real-world applications of circular motion in aviation
USEFUL FOR

Physics students, aviation enthusiasts, and anyone interested in understanding the dynamics of circular motion and forces acting on objects in flight.

Bensky
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Homework Statement


A pilot flies an airplane in a vertical circular loop at a constant speed of v = 160 m/s. If the pilot's apparent weight at the top of the loop is one-third of his true weight on the ground, find the radius R of the plane's circular path.

Answer: R= 1960m


Homework Equations


F_net = ma
a_normal = v^2 / R


The Attempt at a Solution


Top of the loop
-----------------------
mg - N = mv^2 / R
=> N = mg - mv^2/R

mg - mv^2/R = (1/3) * mg
g - v^2/R = (1/3)g
-25600 / R = (-2/3)g
=> R = 3918.367347 m

This is wrong. The answer should be 1960 m, which is exactly half of my answer strangely enough. I am not seeing what I did wrong here at all, can someone point out where I screwed up?

Thank you
 
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What direction is the normal force of the plane on the pilot? (Realize that he's upside down.)
 
Doc Al said:
What direction is the normal force of the plane on the pilot? (Realize that he's upside down.)

So I guess the normal force should be in the same direction as the weight? Thank you, that did give me the correct answer but I'm confused as to why this is happening or why it matters that he is upside down...I guess I don't fully understand what exactly the normal force is. I've really only seen it used in incline plane problems where it is the force exerted by the "plane" on the object.

EDIT: I think I might understand now. I'm imagining the floor of the plane (which is "above") pressing downward on his feet. Is this why it is in the same direction as the weight?
 
The plane pushes up on the pilot's butt, but since the plane is upside down, that's a downward force. The normal force will be whatever it needs to be to maintain the required acceleration. In this problem, you are told that the pilot's weight is insufficient to keep him moving in that vertical circle at the top of the loop (he's going too fast)--so the seat has to exert additional force to help provide the centripetal acceleration.

Bensky said:
EDIT: I think I might understand now. I'm imagining the floor of the plane (which is "above") pressing downward on his feet. Is this why it is in the same direction as the weight?
Yep!
 
Doc Al said:
The plane pushes up on the pilot's butt, but since the plane is upside down, that's a downward force. The normal force will be whatever it needs to be to maintain the required acceleration. In this problem, you are told that the pilot's weight is insufficient to keep him moving in that vertical circle at the top of the loop (he's going too fast)--so the seat has to exert additional force to help provide the centripetal acceleration.


Yep!

Ok, thanks.

And I know this is not part of the problem, but on the sides of the circle, what would the directions for normal force and weight be?
 
Bensky said:
And I know this is not part of the problem, but on the sides of the circle, what would the directions for normal force and weight be?
The true weight, of course, always points down. If the plane is traveling in a vertical circle at constant speed--not so easy to arrange--then the net force on the plane is always towards the center. The same is true for the pilot. For him to not slide around in the plane, the seat must exert a force to balance his true weight and provide the inward force to keep him in a circle. So the seat must exert a diagonally upward force on him.
 

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