Centrifuge Acceleration Calculations

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SUMMARY

The discussion focuses on calculating centrifuge acceleration in two scenarios: on Earth and Mercury. For Part A, the acceleration at halfway to the end of the centrifuge is determined using the formula a = ω²r, leading to an acceleration of 1.70 g. In Part B, to achieve 4 g on Mercury, where gravity is 0.378 g, the required rpm is derived from the relationship a = ω²r, resulting in n being adjusted to account for the lower gravitational force.

PREREQUISITES
  • Understanding of centripetal acceleration and the formula a = ω²r
  • Familiarity with rotational motion concepts, specifically revolutions per minute (rpm)
  • Basic knowledge of gravitational forces on different celestial bodies
  • Ability to manipulate algebraic equations for solving physics problems
NEXT STEPS
  • Study the derivation and application of the centripetal acceleration formula a = ω²r
  • Learn how to convert between different gravitational forces on various planets
  • Explore the effects of radius changes on acceleration in rotational systems
  • Investigate the relationship between rpm and acceleration in centrifuges
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Students studying physics, particularly those focusing on mechanics and rotational dynamics, as well as educators seeking to clarify concepts related to centrifuge operations and gravitational effects on different planets.

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Homework Statement


A laboratory centrifuge on Earth makes n rpm (rev/min) and produces an acceleration of 3.40 g at its outer end.

Part A: What is the acceleration (in g's) at a point halfway out to the end?

Part B: This centrifuge is now used in a space capsule on the planet Mercury, where gMercury is 0.378 what it is on earth. How many rpm (in terms of n) should it make to produce 4 gMercury at its outer end?

Homework Equations



a = v2/R

The Attempt at a Solution



Well using the equation for centripetal acceleration, I figure if the Radius is half then the acceleration in g's would be double for part A. Is that right? or would it be half?

For part B I'm not exactly sure what to use or do. What kind of equation could I use?

Any help would be great! Thanks so much, really thank you
 
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kser said:

Homework Equations



a = v2/R

since we are given rpm or 'ω', let's use a=ω2r instead.


So you know that at the outer end a= 3.40g=ω2r. Our ω in this case is n

so n2r=3.40g


Now halfway to the end is r/2 and ω is the same so we get now:

a1=n2(r/2) → (n2r)/2=a1

try dividing the two equations in red and get a1/3.40g = "something"
 
what do you mean by "dividing the two equations"? combine them? so a/3.40g = ((n^2r)/2))/n^2r ? I'm sorry, am i just looking into this way too much? I don't get what you're saying. because the way i see it. n is constant so when you half the radius, that also halves the acceleration right?
 
Last edited:
kser said:
what do you mean by "dividing the two equations"? combine them? so a/3.40g = ((n^2r)/2))/n^2r ? I'm sorry, am i just looking into this way too much? I don't get what you're saying. because the way i see it. n is constant so when you half the radius, that also halves the acceleration right?

yes that is what I meant by divide.

For the second part, the 'r' is the same at the outer end. So in terms of 'n' find the r using what happens on Earth. The use amercury=N2r
 
yup. I'm sorry i just don't get it. ugh. this whole mercury part it just not makin sense.

so i find r in terms of n and get: r = 3.4/n^2 <--- is that even right? can't be because then I don't see how that would give me what I'm looking for. i am just not good at this stuf...
 
nevermind! got it. thanks so much!
 

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