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Moment of inertia of bar, perpendicular axis

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The moment of inertia is the rotational equivalent of mass in translational motion. In the case of a rod rotating around an axis perpendicular to its own axis, the simplest case occurs when the rotation takes place around the center of mass.

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Mechanisms

Iframe

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Code
Concept

Mechanisms

ID:(15854, 0)



Moment of inertia for an axis not passing through the center of mass

Description

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When the axis of rotation does not pass through the center of mass (CM), the moment of inertia I can be calculated using the Steiner's Theorem. To do this, we start with the moment of inertia with respect to the center of mass, for example:

• For a bar with a perpendicular axis, it is calculated

I_{CM} =\displaystyle\frac{1}{12} m l ^2



• For a cylinder with a perpendicular axis, it is calculated

I_{CM} =\displaystyle\frac{1}{12} m ( h ^2+3 r_c ^2)



• For a cylinder with a parallel axis, it is calculated

I_{CM} =\displaystyle\frac{1}{2} m r_c ^2



• For a parallelepiped, it is calculated

I_{CM} =\displaystyle\frac{1}{12} m ( a ^2+ b ^2)



• For a cube, it is calculated

I_{CM} =\displaystyle\frac{1}{6} m a ^2



• For a sphere, it is calculated

I_{CM} =\displaystyle\frac{2}{5} m r_e ^2



Then, the product of mass and the square of the distance between the axis of rotation and the center of mass is added using

I = I_{CM} + m d ^2

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Bar that rotates around an axis \perp

Image

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A bar with mass m and length l rotating around its center, which coincides with the center of mass:

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Model

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Parameters

Symbol
Text
Variable
Value
Units
Calculate
MKS Value
MKS Units
m
m
Body mass
kg
\alpha_0
alpha_0
Constant Angular Acceleration
rad/s^2
d
d
Distance Center of Mass and Axis
m
\theta_0
theta_0
Initial Angle
rad
\omega_0
omega_0
Initial Angular Speed
rad/s
l
l
Length of the Bar
m
I_{CM}
I_CM
Moment of Inertia at the CM of a thin Bar, perpendicular Axis
kg m^2
I
I
Moment of inertia for axis that does not pass through the CM
kg m^2
r
r
Radio
m
t_0
t_0
Start Time
s
T
T
Torque
N m

Variables

Symbol
Text
Variable
Value
Units
Calculate
MKS Value
MKS Units
\theta
theta
Angle
rad
\omega
omega
Angular Speed
rad/s
F
F
Force
N
t
t
Time
s

Calculations


First, select the equation: to , then, select the variable: to
I = I_CM + m * d ^ 2 I_CM = m * l ^ 2 / 12 omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 T = r * F theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 )thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT

Calculations

Symbol
Equation
Solved
Translated

Calculations

Symbol
Equation
Solved
Translated

Variable Given Calculate Target : Equation To be used
I = I_CM + m * d ^ 2 I_CM = m * l ^ 2 / 12 omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 T = r * F theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 )thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT




Equations

#
Equation

I = I_{CM} + m d ^2

I = I_CM + m * d ^ 2


I_{CM} =\displaystyle\frac{1}{12} m l ^2

I_CM = m * l ^ 2 / 12


\omega = \omega_0 + \alpha_0 ( t - t_0 )

omega = omega_0 + alpha_0 * ( t - t_0 )


T = I \alpha_0

T = I * alpha


T = r F

T = r * F


\theta = \theta_0 + \omega_0 ( t - t_0 )+\displaystyle\frac{1}{2} \alpha_0 ( t - t_0 )^2

theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2


\theta = \theta_0 +\displaystyle\frac{ \omega ^2- \omega_0 ^2}{2 \alpha_0 }

theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 )

ID:(15859, 0)



Moment of inertia of bar length l axis \perp

Equation

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The moment of inertia of a rod rotating around a perpendicular (\perp) axis passing through the center is obtained by dividing the body into small volumes and summing them:

I =\displaystyle\int_V r ^2 \rho dV



resulting in

I_{CM} =\displaystyle\frac{1}{12} m l ^2

m
Body mass
kg
6150
l
Length of the Bar
m
6151
I_{CM}
Moment of Inertia at the CM of a thin Bar, perpendicular Axis
kg m^2
5323
omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 I = I_CM + m * d ^ 2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 ) T = r * F I_CM = m * l ^ 2 / 12thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT

.

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Steiner theorem

Equation

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The moment of inertia for axis that does not pass through the CM (I) can be calculated using the moment of Inertia Mass Center (I_{CM}) and adding the moment of inertia of the body mass (m) as if it were a point mass at the distance Center of Mass and Axis (d):

I = I_{CM} + m d ^2

m
Body mass
kg
6150
d
Distance Center of Mass and Axis
m
5285
I
Moment of inertia for axis that does not pass through the CM
kg m^2
5315
I_{CM}
I_{CM}
Moment of Inertia at the CM of a thin Bar, perpendicular Axis
kg m^2
5323
omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 I = I_CM + m * d ^ 2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 ) T = r * F I_CM = m * l ^ 2 / 12thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT

ID:(3688, 0)



Torque for constant moment of inertia

Equation

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In the case where the moment of inertia is constant, the derivative of angular momentum is equal to

L = I \omega



which implies that the torque is equal to

T = I \alpha_0

T = I \alpha

\alpha
\alpha_0
Constant Angular Acceleration
rad/s^2
5298
I
I
Moment of inertia for axis that does not pass through the CM
kg m^2
5315
T
Torque
N m
4988
omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 I = I_CM + m * d ^ 2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 ) T = r * F I_CM = m * l ^ 2 / 12thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT

Since the moment is equal to

L = I \omega



it follows that in the case where the moment of inertia doesn't change with time,

T=\displaystyle\frac{dL}{dt}=\displaystyle\frac{d}{dt}(I\omega) = I\displaystyle\frac{d\omega}{dt} = I\alpha



which implies that

T = I \alpha

.

This relationship is the equivalent of Newton's second law for rotation instead of translation.

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Simple torque - force relationship

Equation

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Since the relationship between angular momentum and torque is

L = r p



its temporal derivative leads us to the torque relationship

T = r F

F
Force
N
4975
r
Radio
m
9884
T
Torque
N m
4988
omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 I = I_CM + m * d ^ 2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 ) T = r * F I_CM = m * l ^ 2 / 12thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT

Si se deriva en el tiempo la relación para el momento angular

L = r p



para el caso de que el radio sea constante

T=\displaystyle\frac{dL}{dt}=r\displaystyle\frac{dp}{dt}=rF



por lo que

T = r F

The body's rotation occurs around an axis in the direction of the torque, which passes through the center of mass.

ID:(4431, 0)



Angular velocity with constant angular acceleration

Equation

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With the constant Angular Acceleration (\alpha_0), the angular Speed (\omega) forms a linear relationship with the time (t), incorporating the variables the initial Angular Speed (\omega_0) and the start Time (t_0) as follows:

\omega = \omega_0 + \alpha_0 ( t - t_0 )

\omega
Angular Speed
rad/s
6068
\alpha_0
Constant Angular Acceleration
rad/s^2
5298
\omega_0
Initial Angular Speed
rad/s
5295
t_0
Start Time
s
5265
t
Time
s
5264
omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 I = I_CM + m * d ^ 2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 ) T = r * F I_CM = m * l ^ 2 / 12thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT

If we assume that the mean Angular Acceleration (\bar{\alpha}) is constant, equivalent to the constant Angular Acceleration (\alpha_0), then the following equation applies:

\bar{\alpha} = \alpha_0



Therefore, considering the difference in Angular Speeds (\Delta\omega) along with the angular Speed (\omega) and the initial Angular Speed (\omega_0):

\Delta\omega = \omega - \omega_0



and the time elapsed (\Delta t) in relation to the time (t) and the start Time (t_0):

\Delta t \equiv t - t_0



the equation for the mean Angular Acceleration (\bar{\alpha}):

\bar{\alpha} \equiv \displaystyle\frac{ \Delta\omega }{ \Delta t }



can be expressed as:

\alpha_0 = \alpha = \displaystyle\frac{\Delta \omega}{\Delta t} = \displaystyle\frac{\omega - \omega_0}{t - t_0}



Solving this, we obtain:

\omega = \omega_0 + \alpha_0 ( t - t_0 )

This equation represents a straight line in the angular velocity versus time plane.

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Angle at Constant Angular Acceleration

Equation

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Given that the total displacement corresponds to the area under the angular velocity versus time curve, in the case of a constant Angular Acceleration (\alpha_0), it is determined that the displacement the angle (\theta) with the variables the initial Angle (\theta_0), the time (t), the start Time (t_0), and the initial Angular Speed (\omega_0) is as follows:

\theta = \theta_0 + \omega_0 ( t - t_0 )+\displaystyle\frac{1}{2} \alpha_0 ( t - t_0 )^2

\theta
Angle
rad
6065
\alpha_0
Constant Angular Acceleration
rad/s^2
5298
\theta_0
Initial Angle
rad
5296
\omega_0
Initial Angular Speed
rad/s
5295
t_0
Start Time
s
5265
t
Time
s
5264
omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 I = I_CM + m * d ^ 2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 ) T = r * F I_CM = m * l ^ 2 / 12thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT

In the case of the constant Angular Acceleration (\alpha_0), the angular Speed (\omega) as a function of the time (t) follows a linear relationship with the start Time (t_0) and the initial Angular Speed (\omega_0) in the form of:

\omega = \omega_0 + \alpha_0 ( t - t_0 )



Given that the angular displacement is equal to the area under the angular velocity-time curve, in this case, one can add the contributions of the rectangle:

\omega_0(t-t_0)



and the triangle:

\displaystyle\frac{1}{2}\alpha_0(t-t_0)^2



This leads us to the expression for the angle (\theta) and the initial Angle (\theta_0):

\theta = \theta_0 + \omega_0 ( t - t_0 )+\displaystyle\frac{1}{2} \alpha_0 ( t - t_0 )^2

This expression corresponds to the general form of a parabola.

ID:(3682, 0)



Braking angle as a function of angular velocity

Equation

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In the case of the constant Angular Acceleration (\alpha_0), the function of the angular Speed (\omega) with respect to the time (t), along with additional variables the initial Angular Speed (\omega_0) and the start Time (t_0), is expressed by the equation:

\omega = \omega_0 + \alpha_0 ( t - t_0 )



From this equation, it is possible to calculate the relationship between the angle (\theta) and the initial Angle (\theta_0), as well as the change in angular velocity:

\theta = \theta_0 +\displaystyle\frac{ \omega ^2- \omega_0 ^2}{2 \alpha_0 }

\theta
Angle
rad
6065
\omega
Angular Speed
rad/s
6068
\alpha_0
Constant Angular Acceleration
rad/s^2
5298
\theta_0
Initial Angle
rad
5296
\omega_0
Initial Angular Speed
rad/s
5295
omega = omega_0 + alpha_0 * ( t - t_0 ) T = I * alpha_0 theta = theta_0 + omega_0 *( t - t_0 )+ alpha_0 *( t - t_0 )^2/2 I = I_CM + m * d ^ 2 theta = theta_0 +( omega ^2 - omega_0 ^2)/(2* alpha_0 ) T = r * F I_CM = m * l ^ 2 / 12thetaomegamalpha_0dFtheta_0omega_0lI_CMIrt_0tT


If we solve for time in the equation of the angular Speed (\omega) that includes the variables the initial Angular Speed (\omega_0), the time (t), the start Time (t_0), and the constant Angular Acceleration (\alpha_0):

\omega = \omega_0 + \alpha_0 ( t - t_0 )



we obtain the following expression for time:

t - t_0 = \displaystyle\frac{\omega - \omega_0}{\alpha_0}



This solution can be substituted into the equation to calculate the angle (\theta) using the initial Angle (\theta_0) as follows:

\theta = \theta_0 + \omega_0 ( t - t_0 )+\displaystyle\frac{1}{2} \alpha_0 ( t - t_0 )^2



which results in the following equation:

\theta = \theta_0 +\displaystyle\frac{ \omega ^2- \omega_0 ^2}{2 \alpha_0 }

ID:(4386, 0)