Fluid MechanicsQuestion about the Differential Energy Equation

In summary: I see. So the 'case' is that the divergence of the vector velocity (div(v)) represents the continuity equation for a 3D incompressible flow. Got it.
  • #1
Saladsamurai
3,020
7
I am going through the derivation in my text and I have reached a line that makes absolutely no sense to me. I cannot see the correlation between one line and the next and it has led me to believe that it is either an error or just bad editing/wording.

We are at the point where the energy equation has been completely derived, yielding:

[tex]\rho\frac{d\hat{u}}{dt}+p(\nabla\cdot\vec{V}) = \nabla\cdot(k\nabla T) +\Phi \qquad (1)[/tex]​

where [itex]\Phi[/itex] is the viscous work-dissipation function.

He then says that
since (1) if often too difficult to analyze, it is cstomary to make the following approximations: [itex]d\hat{u}\approx c_vdT \qquad & \qqaud c_v,\mu,k,\rho\approx\text{constant}[/itex]

Okay, that's great. Here, the next line is where I get all messed up:

Equation 9 then takes the simpler form, for [itex]\nabla\cdot\vec{V}=0[/itex],

[tex]\rho c_v\frac{dT}{dt}=k\nabla^2T+\Phi[/tex]​

What?! How does [itex]d\hat{u}\approx c_vdT \qquad & \qqaud c_v,\mu,k,\rho\approx\text{constant}[/itex] imply that [itex]\nabla\cdot\vec{V}=0[/itex] ?

Or are the two completely unrelated and the wording only makes it seem like the 2 statements follow logically.

Is the [itex]\nabla\cdot\vec{V}=0[/itex] 'case' another condition that he is imposing on (1) in addition to the conditions [itex]d\hat{u}\approx c_vdT \qquad & \qqaud c_v,\mu,k,\rho\approx\text{constant}[/itex]?

I am confused :confused:

Any insight is appreciated as always :smile:
 
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  • #2
The two statements are unrelated, AFAIK. Two separate simplifications.
 
  • #3
Andy Resnick said:
The two statements are unrelated, AFAIK. Two separate simplifications.

Yeah it's weird. He goes on a few lines later to talk about the special case where the fuid is at rest. But in the above, even though [itex]\nabla\cdot\vec{V}=0[/itex], that does not mean that the fluid is at rest since [itex]dT/dt \ne0[/itex], which contains velocity components.

So I don't see when we would have [itex]\nabla\cdot\vec{V}=0[/itex] AND [itex]dT/dt \ne0[/itex].

What special case is that? And why would he not explicitly give the details as to what that meant physically? Like when the fluid flows over kittens or something...what is the 'special case' ?
 
  • #4
Saladsamurai said:
Yeah it's weird. He goes on a few lines later to talk about the special case where the fuid is at rest. But in the above, even though [itex]\nabla\cdot\vec{V}=0[/itex], that does not mean that the fluid is at rest since [itex]dT/dt \ne0[/itex], which contains velocity components.

They left out an equation.

[itex] {\partial \rho \over \partial t} + \nabla \cdot (\rho \mathbf{V}) = 0[/itex]

If you set \rho constant then you get [itex]\nabla\cdot\vec{V}=0[/itex]
 
  • #5
twofish-quant said:
They left out an equation.

[itex] {\partial \rho \over \partial t} + \nabla \cdot (\rho \mathbf{V}) = 0[/itex]

If you set \rho constant then you get [itex]\nabla\cdot\vec{V}=0[/itex]


Oh wow. Nice catch twofish-quant :thumbsup: Maybe he did not 'leave it out;' maybe his intent was for the reader to really 'flex' that brain.

This must be what he meant back in the beginning of the chapter on differential relations. He said something to the effect of "<paraphrasing> we must always return to the continuity equation else our results will be most likely be nonsensical..."

It never occurred to me that just because the energy equation or momentum equation looks mathematically sound that it might not be physically sound.

Thanks! :smile:
 
  • #6
Hi, I am trying to derive the full energy equation for a fluid (rho du/dt + P grad V=del dot (kgrad T) + the viscous dissipation function. I understand almost the entire derivation but my texts leave out a few steps. Instead of asking the specifics since I am not well versed with the equation editor, can someone post the entire step by step derivation? Thanks
 
  • #7
Saladsamurai said:
I am going through the derivation in my text and I have reached a line that makes absolutely no sense to me. I cannot see the correlation between one line and the next and it has led me to believe that it is either an error or just bad editing/wording.

We are at the point where the energy equation has been completely derived, yielding:

[tex]\rho\frac{d\hat{u}}{dt}+p(\nabla\cdot\vec{V}) = \nabla\cdot(k\nabla T) +\Phi \qquad (1)[/tex]​

where [itex]\Phi[/itex] is the viscous work-dissipation function.

He then says that


Okay, that's great. Here, the next line is where I get all messed up:

[/CENTER]

What?! How does [itex]d\hat{u}\approx c_vdT \qquad & \qqaud c_v,\mu,k,\rho\approx\text{constant}[/itex] imply that [itex]\nabla\cdot\vec{V}=0[/itex] ?

Or are the two completely unrelated and the wording only makes it seem like the 2 statements follow logically.

Is the [itex]\nabla\cdot\vec{V}=0[/itex] 'case' another condition that he is imposing on (1) in addition to the conditions [itex]d\hat{u}\approx c_vdT \qquad & \qqaud c_v,\mu,k,\rho\approx\text{constant}[/itex]?

I am confused :confused:

Any insight is appreciated as always :smile:
simply the the the divergence of the vector velocity (div(v)) THIS QUANTITY REPRESENT THE CONTINUITY EQUATION FOR A 3D INCOMPRESSIBLE FLOW.
Go back to the continuity equation and you see that Prof Franl white he made a derivation in catesian coordinate and cylindrical coordinates system for an unsteady compressble conditions.
but if we expande the the contnuity , and we assume that the flow is incompressble we get exactely the div(V)=nabla dot( V), nabla is a diferential operator when it operate on vector as grad(v) has no sense, but when it dot the result is a scalar function.
*iF YOU NEDD A DETAILLED DERIVATION OF ALL THE EQUATION , AND THE SCALLING FACTORS, IN ORDER TO FIND THE CONTINUITY IN CYLINDRICAL AND SPHERICAL COORDINATES SEND ME A MESSAGE, AND I WILL SEND YOU THE FULL DETAILLED DERIVATIO. MY EMAIL=(london_maurice@hotmail.com)
 
  • #8
du=Cvdt this is the internal energy for a caloricaly, perfect gas. mu is the viscosity,k is the heat conduction,rho is the density.
 
  • #9
But i don't understand one things here Salds how did you get into this step without having problem with the steps before?
 

FAQ: Fluid MechanicsQuestion about the Differential Energy Equation

What is the differential energy equation in fluid mechanics?

The differential energy equation in fluid mechanics is a mathematical representation of the conservation of energy in a fluid system. It describes how the total energy of the fluid changes as it flows through a system and accounts for factors such as pressure, velocity, and internal energy.

How is the differential energy equation derived?

The differential energy equation is derived from the principles of conservation of mass, momentum, and energy. It can also be derived from the Navier-Stokes equations, which govern the motion of fluids.

What is the significance of the differential energy equation in fluid mechanics?

The differential energy equation is important in fluid mechanics because it allows us to predict the behavior of fluids in a wide range of systems, from pipes and pumps to turbines and aircraft wings. It also provides a basis for understanding and optimizing fluid flow in engineering applications.

What are the assumptions made in the differential energy equation?

The differential energy equation assumes that the fluid is incompressible, inviscid (no viscosity), and in steady-state (no changes in time). It also assumes that there are no external forces acting on the fluid other than pressure and gravity.

How is the differential energy equation applied in real-world problems?

The differential energy equation is used in conjunction with other equations and principles in fluid mechanics to solve a variety of real-world problems. For example, it can be used to calculate the flow rate of a fluid through a pipe or the lift force on an airplane wing. It is also used in the design and analysis of hydraulic systems and turbines.

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