A question on centrifugal artifical gravity

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To maintain Earth gravity on the interior surface of a hollow cylindrical object with a diameter of seven miles, it needs to spin at a specific angular velocity. The radius of the cylinder is 3.5 miles, or approximately 5607 meters. The centripetal acceleration required to simulate Earth gravity (approximately 9.81 m/s²) must equal the centripetal acceleration at the edge of the cylinder, given by the formula a_edge = R * ω². By rearranging this equation to solve for angular velocity (ω), it is determined that the cylinder must rotate at about 0.40 revolutions per minute. This equates to a revolution every 2.5 minutes, providing the necessary artificial gravity for occupants inside the cylinder.
grubbyknickers
How fast would a hollow cylindrical object seven miles in diameter need to spin to maintain Earth gravity on the interior surface?
 
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grubbyknickers said:
How fast would a hollow cylindrical object seven miles in diameter need to spin to maintain Earth gravity on the interior surface?

Welcome to the PF.

What is the context of the question? Is this for schoolwork? What do you know already about centriptal forces?
 
the question does not relate to schoolwork, I'm working on a science fiction novel and my math skills are inferior so I can't crack a book and easily solve the equation myself.
I need to know the rpm the cylinder would need to spin at to maintain normal Earth gravity (would it be a four minute revolution, a half hour revolution?).
 
Do you recognise the equation ω2r for calculating centripetal acceleration
Also, when you come to do the calculation I would suggest that you give the radius in metres rather than miles.
 
If the space station is 7 miles in diameter, it is 3.5 miles in radius.

If we assume that we want to feel Earth-level artificial gravity at this distance from the center, we want the centripedal acceleration of a point on this cylinder to be the same as the acceleration due to gravity. In short,

a_{edge} = g
but
a_{edge} = R \omega^{2}
where R is the radius of the station (3.5 miles or 5607 meters) and omega is the angular velocity of the space station in radians per second.

Then we solve for \omega, finding that
\omega=\sqrt{\frac{g}{R}}
so that \omega is about 6.64thousandths of a revolution per second or about 0.40 revolutions per minute.
 
hope that helps:)
 
4/10 revolutions per minute means 10/4 minutes per revolution or about 2 1/2 minutes per revolution
 
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