mridul
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Its as simple as this .actually mass of the body does not change with time so it is a constant .Now the constant comes out of the factor that's why.sorry for bad eng
The discussion centers on the application of the product rule in the context of Newton's second law when dealing with variable mass systems. It is established that the expression d/dt(mv) = mdv/dt + vdm/dt is incorrect due to its violation of Galilean invariance. Specifically, a variable-mass object with zero force in one inertial frame may exhibit non-zero force in another, highlighting the necessity of accounting for mass changes in momentum calculations. The conversation emphasizes the importance of conservation laws and the implications of mass variability on classical mechanics.
PREREQUISITESPhysics students, educators, and professionals interested in classical mechanics, particularly those exploring the complexities of variable mass systems and their implications on Newtonian physics.
Halliday; Resnick. Physics. 1. p. 199. ISBN 0-471-03710-9. It is important to note that we cannot derive a general expression for Newton's second law for variable mass systems by treating the mass in F = dP/dt = d(Mv) as a variable. [...] We can use F = dP/dt to analyze variable mass systems only if we apply it to an entire system of constant mass having parts among which there is an interchange of mass.
If you insist.conscience said:@haruspex , do you mind giving your views on this topic .
You appear to have misunderstood my example. Perhaps I should have written "becomes detached from". The dust particle, as such, does not gain momentum from the ball. It keeps exactly the momentum it had, as does the ball. They are simply no longer joined. The problem comes from defining the system as "ball plus whatever is attached". When the particle becomes detached, this system loses momentum, yet no forces were involved.vanhees71 said:When the dust particle falls of it gains momentum relative to the ball and thus the ball also gets a recoil,
Well, that doesn't make sense. Either the particle changes it's momentum relative to the ball or it still is comoving with the ball. You cannot loose momentum without a force, and total momentum is conserved. For the rocket, I've shown both approaches in this thread above. For this purpose you need to consider only the center of mass of the fuel and of the rocket as an effective description of the closed system, and total momentum is conserved, which leads to the equation of motion ("rocket equation") for the rocket.haruspex said:You appear to have misunderstood my example. Perhaps I should have written "becomes detached from". The dust particle, as such, does not gain momentum from the ball. It keeps exactly the momentum it had, as does the ball. They are simply no longer joined. The problem comes from defining the system as "ball plus whatever is attached". When the particle becomes detached, this system loses momentum, yet no forces were involved.
I believe the same issue applies to the rocket if you try to define the system as rocket plus unused fuel.
One can gain or lose momentum from a system by re-drawing the boundaries around the system. Of course, that means that the system is not closed. That is the point.vanhees71 said:Well, that doesn't make sense. Either the particle changes it's momentum relative to the ball or it still is comoving with the ball. You cannot loose momentum without a force, and total momentum is conserved. For the rocket, I've shown both approaches in this thread above. For this purpose you need to consider only the center of mass of the fuel and of the rocket as an effective description of the closed system, and total momentum is conserved, which leads to the equation of motion ("rocket equation") for the rocket.
That's what this thread is all about, that if you apply the standard equationsvanhees71 said:Well, that doesn't make sense. Either the particle changes it's momentum relative to the ball or it still is comoving with the ball. You cannot loose momentum without a force, and total momentum is conserved. For the rocket, I've shown both approaches in this thread above. For this purpose you need to consider only the center of mass of the fuel and of the rocket as an effective description of the closed system, and total momentum is conserved, which leads to the equation of motion ("rocket equation") for the rocket.