I Do objects always rotate around center of mass?

Click For Summary
Objects do not always rotate around their center of mass (CoM); the axis of rotation can vary based on external forces and conditions. For example, when an airplane or boat adjusts its rudder, it may rotate around a point far from its CoM, influenced by aerodynamic or hydrodynamic forces. The concept of rotation is complex, as any rigid body can be described as rotating around any point, but this does not imply that it rotates solely around the CoM. The instantaneous center of rotation can change and is not fixed, depending on the forces acting on the object. Understanding the dynamics of rotation requires recognizing that while the CoM plays a significant role in motion analysis, it is not the exclusive point of rotation.
  • #31
Lnewqban said:
quote from text:

"The side force (F) is applied through the center of pressure of the vertical stabilizer which is some distance (L) from the aircraft center of gravity. This creates a torque

T = F * L

on the aircraft and the aircraft rotates about its center of gravity."So people who read this conclude that object always rotate around c.g./com....Then comes to this forum and ask questions. I think it has 1000 questions in this forum at this topic
 
Physics news on Phys.org
  • #32
For a plane it is reasonable to describe change of heading in a turn as "rotation" (but i've never heard it), but for the actual stick and rudder flying it's more commonly defined as rotation about the center of mass:

https://en.m.wikipedia.org/wiki/Aircraft_principal_axes

Of course, when a pilot says "rotate!" most often It's about the axle of the main landing gear at takeoff.

So I agree it depends.
 
  • #33
PeroK said:
What's the definition of rotate?
In my brain, rotate mean circular motion of object around axis that passes anywhere inside object geometry, if axis is out of object geometry than I call it revolve.
That seems logic to me.

Is this Ok?
 
  • #34
user079622 said:
In my brain, rotate mean circular motion of object around axis that passes anywhere inside object geometry, if axis is out of object geometry than I call it revolve.
That seems logic to me.

Is this Ok?
Yes.
 
  • #35
PeroK said:
Yes.
Problem is when airplane move elevator, he revolve around some axis far away from him and rotate around some axis that passes through airplane body, but it turn out that dont have to be through c.g.?
 
  • #36
user079622 said:
In my brain, rotate mean circular motion of object around axis that passes anywhere inside object geometry, if axis is out of object geometry than I call it revolve.
Why invent more names than needed based on where the axis is?

- rotation is change of orientation
- translation is change of position

They can be combined, but that requires choosing a reference point. Choosing the center of mass often makes the math of applying Newton's Laws simpler. That's why it's often used.
 
  • Like
Likes FactChecker, russ_watters and nasu
  • #37
user079622 said:
In my brain, rotate mean circular motion of object around axis that passes anywhere inside object geometry, if axis is out of object geometry than I call it revolve.
That seems logic to me.

Is this Ok?
That is fine, but the issue is that the axis is not unique. Consider a wheel. You can say that it rotates about the axle, or that it rotates about the contact point, or indeed about any other point whether on or off the wheel.

user079622 said:
Problem is when airplane move elevator, he revolve around some axis far away from him and rotate around some axis that passes through airplane body, but it turn out that dont have to be through c.g.?
Correct. It can be considered about any point, it is not restricted to the cg
 
  • Like
Likes nasu
  • #38
Dale said:
That is fine, but the issue is that the axis is not unique. Consider a wheel. You can say that it rotates about the axle, or that it rotates about the contact point, or indeed about any other point whether on or off the wheel.

Correct. It can be considered about any point, it is not restricted to the cg
But..
If we dont know that airplane rotate around cg, then we can put lift force in front of cg and plane will unstable and kill someone.

So we must know what is real axis around which will plane rotate when disturbance comes.
I dont know what is name of this point/axis but I know engineers must know this position.
Is this called instant center of rotation?

Plane fly in straight line above runway and when gust hit him from side, he rotate into wind.
Where is axis of rotation? It can be anywhere?
 
Last edited:
  • #39
user079622 said:
If we dont know that airplane rotate around cg, then we can put lift force in front of cg and plane will unstable and kill someone.
This is simply not true. The axis of rotation is part of the analysis. It has no bearing on the stability of the air frame.

user079622 said:
So we must know what is real axis around which will plane rotate when disturbance comes
You claim this, but it is simply false.

user079622 said:
I dont know what is name of this point/axis but I know engineers must know this position.
Is this called instant center of rotation?
I don’t know it either. If you do find the term it would be useful. I am sure that the engineers have a clear definition for it.

user079622 said:
Where is axis of rotation? It can be anywhere?
Yes.
 
  • #40
@user079622

This is just a mathematical fact of rigid body motion, purely kinematically. It is just the way that rigid body motion behaves mathematically.

Suppose I have a rigid disk which is spinning about its center of mass. At a given instant I can plot the velocity of each point on the disk as follows:

View attachment 319993

The formula for the velocity field is ##\vec v=(y,-x)##. This is rotation around the center, as expected.

However, suppose instead of a disk rotating, we have a wheel rolling. Kinematically these are the same motion in different reference frames. Then at any given instant I can plot the velocity of each point on the wheel as follows:

View attachment 319994

The formula for the velocity field is ##\vec v=(y,-x)+(1,0)##. Notice that this motion is also a pure rotation, but about the bottom of the wheel, the point that it contacts the ground. Again, this is kinematically identical to the disk rotating about the center in a different reference frame.

These two points are not special. In fact, for any point on the wheel you can pick a reference frame where that point is momentarily at rest. When you do so the motion is as follows:

View attachment 319996

The formula for this velocity field is ##\vec v=(y,-x)+(0,0.7)##. Notice again that this motion is momentarily a pure rotation about the chosen point which happens to be ##(0.7,0)##.

This is a general feature of rigid body motion. You can always decompose the velocity of the material points in a rigid body into a pure rotation about any point and a rigid translation.
 
  • Like
Likes jbriggs444 and nasu
  • #41
user079622 said:
quote from text:

"The side force (F) is applied through the center of pressure of the vertical stabilizer which is some distance (L) from the aircraft center of gravity. This creates a torque

T = F * L

on the aircraft and the aircraft rotates about its center of gravity."So people who read this conclude that object always rotate around c.g./com....Then comes to this forum and ask questions. I think it has 1000 questions in this forum at this topic
The center of mass of the airplane must follow Newton’s laws.
It would follow a rectilinear trajectory, unless forced to deviate from that natural traslation.
The external force on the rudder is not that force; therefore, the plane initially yaws (rotates around the CM until finding a position of balance) and its CM continues moving on a straight line.
That does not last long, as other aerodynamic forces appear.

For example, the tail is higher than the CM, reason for which the plane also rolls (rotates sideways).
Once it is rolled and crabing, one wing receives more airstream than the other, and more inestability appears.
Both additional movements must be controlled by ailerons, which may induce additional yaw.

In order to follow a horizontal circular trajectory, the CM must be forced to do so by a centripetal horizontal force, which is normally a horizontal component of the lift vector.
That vector is tilted because the plane has been rolled and pitched up simultaneously.

As you can see, a sequence of several torques and rotations appear for a simple maneuver.
 
  • #42
user079622 said:
quote from text:

"The side force (F) is applied through the center of pressure of the vertical stabilizer which is some distance (L) from the aircraft center of gravity. This creates a torque

T = F * L

on the aircraft and the aircraft rotates about its center of gravity."So people who read this conclude that object always rotate around c.g./com....Then comes to this forum and ask questions. I think it has 1000 questions in this forum at this topic
The fact that it rotates about one point does not exclude rotation about another point. There is no contradiction.
However, what the existence of a torque about the CG actually implies is that there will be some angular acceleration about this point. If there was no previous rotation about CG, obviously it will start to rotate.
And by the way, the same force will have a torque about many other points on the airplane. It's just easier to analyze the dynamics by using the COM.
 
  • Like
Likes Dale
  • #43
Wikipedia says that for a free-floating (unattached) object, the axis of rotation is commonly around its center of mass. https://en.wikipedia.org/wiki/Rotational_energy

Does this mean there are exceptions where some objects' axis of rotation does not rotate around their center of mass in the case of free-floating?
 
  • #44
alan123hk said:
Does this mean there are exceptions where some objects' axis of rotation does not rotate around their center of mass in the case of free-floating?
It means that there are exceptions where the people analyzing the scenario choose to analyze its rotation about a different axis. For instance, they might analyze the moon as rotating about the barycenter instead of its own axis.
 
  • Like
Likes alan123hk
  • #45
Got it, thank you for your explanation.
 
  • Like
Likes Dale
  • #46
alan123hk said:
Wikipedia says that for a free-floating (unattached) object, the axis of rotation is commonly around its center of mass. https://en.wikipedia.org/wiki/Rotational_energy
What it actually means is that if you want to use the moment of inertia around the CoM (as it is commonly provided), then you also have to use the rotation around the CoM to compute the rotational KE. But you could use any other point, as long as you stay consistent. You will get the same total KE, but a different composition of linear vs. rotational KE.
 
  • Like
Likes PeroK and alan123hk
  • #47
user079622 said:
Plane fly in straight line above runway and when gust hit him from side, he rotate into wind.
Where is axis of rotation? It can be anywhere?
Yes, one can put the axis anywhere for analysis, but it is often not practical to do so. In this case, since the plane is moving and rotating, even the instantaneous axis of rotation is not the CoM, and might even be somewhere outside the plane.
 
  • #48
A.T. said:
Yes, one can put the axis anywhere for analysis, but it is often not practical to do so. In this case, since the plane is moving and rotating, even the instantaneous axis of rotation is not the CoM, and might even be somewhere outside the plane.
If force act at 90degress at the end of stick in free space, will he rotate around CoM and CoM will translate in straight line?
 
  • #49
Dale said:
This is simply not true. The axis of rotation is part of the analysis. It has no bearing on the stability of the air frame.

You claim this, but it is simply false.

I don’t know it either. If you do find the term it would be useful. I am sure that the engineers have a clear definition for it.

Yes.
When gust of wind hit plane from side, it act at lateral center of pressure which is for sure behind c.g. because of big tail surface.
Plane will do some small side slip so we have another small aerodynamic force at center of lateral pressure but from opposite side.

thrust force from left and right engines are equal so they dont cause any toruque.

So we have aero side force from gust minus aero side force side slip and CoM which resist to accelarate if something want to do it.Free body diagram , top view
This side force will translate plane c.g. downwind and rotate plane into wind around instant axis that passes through c.g
Is it ok?
Untitled.png
 
  • Like
Likes Dale
  • #50
user079622 said:
If force act at 90degress at the end of stick in free space, will he rotate around CoM and CoM will translate in straight line?
That is one possible way to desctibe the motion, but not the only one.
 
  • #51
A.T. said:
That is one possible way to desctibe the motion, but not the only one.
But is instant axis of rotation through CoM?
 
Last edited:
  • #52
user079622 said:
But is instant axis of rotation through CoM? In another words, can single force make object to rotate around com?
The "instantaneous axis of rotation" is the axis that is momentarily motionless.

However, "motionless" is always relative to a chosen frame of reference. Change the frame of reference and you change which axis is "motionless".

It is quite convenient to adopt the rest frame of the stick's center of mass. So convenient that we tend to do so without even thinking about it. That is why we tend to think of the stick as rotating about its center of mass.
 
  • Like
Likes user079622
  • #53
user079622 said:
Free body diagram , top view
This side force will translate plane c.g. downwind and rotate plane into wind around instant axis that passes through c.g
Is it ok?
Yes, that is all good
 
  • #54
jbriggs444 said:
The "instantaneous axis of rotation" is the axis that is momentarily motionless.

However, "motionless" is always relative to a chosen frame of reference. Change the frame of reference and you change which axis is "motionless".

It is quite convenient to adopt the rest frame of the stick's center of mass. So convenient that we tend to do so without even thinking about it. That is why we tend to think of the stick as rotating about its center of mass.
Is any difference if my force is some rocket engine at the end of stik working all the time or if my force is short impulse ,when I hit end of stick with hammer?
In first case we have continous external force in second case just first "second" one hit with external force and after that no external force
Will stick behave the same in both case in free space?
 
  • #55
Dale said:
Yes, that is all good
So I dont see any difference with stick in free space and my free body diagram of gust/plane, stick "rotate" around CoM and my plane "rotate" around c.g.
 
  • #56
A.T. said:
even the instantaneous axis of rotation is not the CoM, and might even be somewhere outside the plane.
Why do you think not at CoM? We have just one side force and plane CoM...
 
  • #57
user079622 said:
So I dont see any difference with stick in free space and my free body diagram of gust/plane, stick "rotate" around CoM and my plane "rotate" around c.g.
Me neither. The difference is in your claims, not in the physics.

In the one where I said it was ok you claimed that it rotates about the cg. That is fine, it does rotate about the cg.

The ones where I objected you were claiming that if it rotates about any other axis there is some problem. That is not fine, if it rotates about the cg then it also rotates about any other parallel axis. That is just a fact of rigid body motion.

The problematic claim is not that it rotates about the cg, the problematic claim is that it only rotates about the cg or that the cg is unique or that if it rotates about another axis then it is unstable, etc.
 
  • Like
Likes nasu
  • #58
Dale said:
Me neither. The difference is in your claims, not in the physics.

In the one where I said it was ok you claimed that it rotates about the cg. That is fine, it does rotate about the cg.

The ones where I objected you were claiming that if it rotates about any other axis there is some problem. That is not fine, if it rotates about the cg then it also rotates about any other parallel axis. That is just a fact of rigid body motion.

The problematic claim is not that it rotates about the cg, the problematic claim is that it only rotates about the cg or that the cg is unique or that if it rotates about another axis then it is unstable, etc.
But that is not valid for instant center of rotation?
I am talking about instant center all the time..
 
  • #59
user079622 said:
But that is not valid for instant center of rotation?
I am talking about instant center all the time..
What is the precise scientific definition of “instant center of rotation”? I don’t know what that means.
 
  • #60
Dale said:
What is the precise scientific definition of “instant center of rotation”? I don’t know what that means.
Nither I.
This is place in universe where in time t1, angular velocity is zero, every particle of this object rotate around this center.
 

Similar threads

  • · Replies 67 ·
3
Replies
67
Views
5K
  • · Replies 10 ·
Replies
10
Views
1K
Replies
117
Views
7K
Replies
6
Views
2K
  • · Replies 15 ·
Replies
15
Views
3K
  • · Replies 4 ·
Replies
4
Views
2K
  • · Replies 8 ·
Replies
8
Views
1K
  • · Replies 49 ·
2
Replies
49
Views
5K
  • · Replies 10 ·
Replies
10
Views
493
Replies
23
Views
3K