Help with Derivation of Centrifugal Force Equation

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The discussion revolves around understanding the derivation of the centrifugal force equation, specifically the transformation of derivatives in rotating reference frames. The original poster struggles with the coordinate transformation equation and how it relates to Newton's second law in a rotating frame. They initially misinterpret the application of the transformation, leading to confusion in deriving acceleration expressions. After receiving clarification, they successfully derive the correct form of the acceleration equation but remain uncertain about the foundational coordinate transformation. The conversation highlights the complexities of applying physics concepts in non-inertial frames and the importance of understanding operator equations.
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Hello world,

I'm trying to understand the derivation of the centrifugal force equation, F_{centrifugal} = - m \omega \times \left( \omega \times r \right). I used these pages to help me in my pursuit:

  • http://observe.arc.nasa.gov/nasa/space/centrifugal/centrifugal6.html"
  • http://en.wikipedia.org/wiki/Rotating_reference_frame"

However, I lack the background to understand either of these articles. This last school year, I completed AP Calculus and first-year high school physics. I understood the material fairly well, but it does not appear to be enough to figure out the concepts discussed here. I will be taking AP Physics, multivariable calculus, and linear algebra next year.

So, off we go:

1.
From the NASA article

We wish to express Newton's second law in a reference frame that rotates uniformly and with angular velocity w (units of radians per second) relative to our inertial reference frame. This is accomplished by applying the coordinate transformation

\left( \frac {d} {dt} \right) _{i} = \left( \frac {d} {dt} \right) _{r} + \omega \times

Uhh... what? The derivative of what with respect to time? Omega times what? It appears this is some sort of a fill-in-the-blanks equation - just down below, they fill the blanks in with r. But can anyone explain the meaning of this equation? Why does it supposedly make sense?

By the way, the "times" symbol, \times, represents the cross product.

2.
From the NASA article again

Upon applying the coordinate transformation a second time, to v_i, we obtain an expression for acceleration a_i in the rotating reference frame:

a_i = a_r + 2 \omega \times v_r + w \times \left( \omega \times r \right)

It appears to me that to obtain a_i, they simply took the derivative of v_i, the equation for which is:

v_i = v_r + \omega \times r.

However, when I do it, I get a different result:

a_i = \frac {d} {dt} \left( v_i \right) = \frac {d} {dt} \left( v_r + \omega \times r \right) =a_r + \omega \times v_r + \alpha \times r

I simply differentiated the expression for v_i, using the product rule for the cross product. Alpha is angular acceleration, which is the derivative of angular speed, omega. What did I do wrong?

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For now, I'll be happy to just understand these 2 problems. I won't even begin about the Wikipedia article (any math-related Wikipedia article has a crushing effect on my self-esteem). If anyone can offer some help, I'll appreciate it highly.
 
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1. is an equation of "operators". The idea is that it is true with any arbitrary function (say "f", "h", "r" or "v_i") placed on the right of all three terms. (At first such equations might make more sense if you always explicitly write in "f(x)" where appropriate, but the other notation is more efficient.)

2. a_i is the rate of change (in the inertial frame) of the velocity (in the inertial frame). The problem is that a_r is supposed to represent the rate of change in the rotating (not inertial) frame of the velocity in the rotating frame, so substitute your eq.(1) for the (inertial frame) differential operator you tried using in your last equation (and note that \alpha = 0).
 
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Thank you for the help. I managed to derive the equation properly:

\left( \frac{d}{dt} \right) _i = \left( \frac{d}{dt} \right) _r + \omega \times

This "transformation" is first applied to r:
\left( \frac{dr}{dt} \right) _i = \left( \frac{dr}{dt} \right) _r + \omega \times r
v_i = v_r + \omega \times r

And then to v_i:
\left( \frac{d}{dt} \left( v_i \right) \right) _i = \left( \frac{d}{dt} \left( v_i \right) \right) _r + \omega \times v_i

Now substitute every v_i on the right side of this equation with v_r + \omega \times r:
\left( \frac{d}{dt} \left( v_i \right) \right) _i = \left( \frac{d}{dt} \left( v_r + \omega \times r \right) \right) _r + \omega \times \left( v_r + \omega \times r \right)

After simplifying, I finally obtained the result I was looking for:
a_i = a_r + 2 \omega \times v_r + \omega \times \left( \omega \times r \right)

Phew!

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Well, everything makes sense, except for the very first step. I'm not sure how they obtained the original coordinate transformation in the first place:

\left( \frac{d}{dt} \right) _i = \left( \frac{d}{dt} \right) _r + \omega \times

I think I understand the concept of "equation of operators" now, but I don't understand why it is what it is. Why is it that a differential change (of something) in the inertial frame is equivalent to the same differential change (of the same something) in the rotating frame plus the angular velocity multiplied by that "something"?

Again, I would appreciate any help. Thank you in advance.
 
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