Different forms of fluid energy conservation equations

In summary, different forms of fluid energy conservation equations describe the principles governing the conservation of energy in fluid systems. These equations encompass various forms, including the Bernoulli equation, which relates pressure, velocity, and height in a flowing fluid, and the first law of thermodynamics, which accounts for energy transfer through heat and work. Other forms include the Navier-Stokes equations, which incorporate viscous effects, and energy equations that consider internal energy changes within the fluid. These formulations are essential for analyzing fluid behavior in engineering applications, ensuring efficient energy management in systems involving fluids.
  • #1
happyparticle
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Homework Statement
Derive the different forms of the continuity equation
Relevant Equations
##\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
##

##\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

##\frac{D}{Dt} \frac{p}{\rho^{\gamma}} = 0
##

##e = \frac{1}{\gamma -1} \frac{p}{\rho}
##
I asked this question about one year ago, but at that time I didn't really understand what I was doing.

After spending a lot of time in this problem, I still fail to get the asked answer.

Starting with ##\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p## I have to derive the following expressions.

##\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

##\frac{D}{Dt} \frac{p}{\rho^{\gamma}} = 0
##

I don't know what I'm doing wrong or what I'm missing, but I couldn't get those expressions.

Here is what I did.
##\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
## (1)

## \frac{De}{Dt} = \frac{\partial}{\partial t} (\frac{P}{(\gamma - 1) \rho}) + (\vec{u} \cdot \nabla) (\frac{P}{(\gamma -1) \rho})## (2)

Replacing (2) into (1) and multiplying both side by ##(\gamma - 1) \rho##
## \frac{\partial p}{\partial t} - \frac{p \partial \rho}{\rho \partial t} + \vec{u} \cdot \nabla p - \frac{p}{\rho} \vec{u} \cdot \nabla \rho + (\gamma -1)p \nabla \cdot \vec{u} = - (\gamma -1) \vec{u} \cdot \nabla p##

Then using the definition of the material derivative.
##\frac{Dc}{Dt} = \frac{\partial c}{\partial t} + \vec{u} \cdot \nabla c##

##\frac{Dp}{Dt} - \frac{P}{\rho} \frac{D\rho}{Dt} + (\gamma -1)p \nabla \cdot \vec{u} = - (\gamma -1) \vec{u} \cdot \nabla p ##

So far there are too much terms on the left hand side. For instance, there are two terms with ##\gamma## and in the final answer there is only one.
 
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  • #2
The continuity equation is [tex]
\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{u}) = 0.[/tex] This can be rewritten as [tex]
\frac{D\rho}{Dt} + \rho \nabla \cdot \vec{u} = 0.[/tex] Your first relevant equation for [itex]De/Dt[/itex] is the conservation of internal energy, which is an independent result.

From [tex]
(\gamma -1 )e\rho = p[/tex] you can take the material derivative of both sides and use the product rule on the left to get an expression for [itex]Dp/Dt[/itex] in terms of [itex]De/Dt[/itex] and [itex]D\rho/Dt[/itex], both of which you already know. Then you can use the quotient rule on [tex]
\frac{D}{Dt}\left(\frac{p}{\rho^\gamma}\right).[/tex]
 
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  • #3
happyparticle said:
##\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##
This equation is the expression for adiabatic reversible expansion or compression of an ideal gas.
happyparticle said:
##\frac{D}{Dt} \frac{p}{\rho^{\gamma}} = 0
##
This can be derived from the previous equation using the continuity equation.
 
  • #4
I don't know where to begin to get this equation ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

I thought I had to start from the conservation of internal energy.
 
  • #5
The last equation is derived by the ideal gas relationship:$$e=C_VT= C_V\frac{pv}{R}$$where v is the molar density ##v=1/\rho## and e is the internal energy per mole. So, $$e=\frac{C_Vp}{\rho R}=\frac{p}{\rho}\frac{1}{\gamma-1}$$

The first equation derives from the adiabatic thermal energy balance equation $$\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-p\nabla \centerdot \vec{u}$$
 
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  • #6
I knew how to get those equations. Here I have to get the second equation, but I don't know where to begin.


As I said, I thought I had to start from the conservation of internal energy.
 
  • #7
happyparticle said:
I knew how to get those equations. Here I have to get the second equation, but I don't know where to begin.


As I said, I thought I had to start from the conservation of internal energy.
The final equation in my post is the energy conservation equation.
 
  • #8
Chestermiller said:
The final equation in my post is the energy conservation equation.
Exactly, @pasmith wrote it. However I thought I could get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
## from it.

In my first post I started with the energy conservation equation to get the expression above. However, I think they are independent. Basically, I'm trying to understand how to get ##\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0##, then as you said, I can derive ##
\frac{D}{Dt} \frac{p}{\rho^{\gamma}} = 0
## from it.

I think I understand...
The term ##\nabla P## is 0 for the energy conservation equation and then from there I can get what I'm looking for. Am I correct?
 
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  • #9
happyparticle said:
Exactly, @pasmith wrote it. However I thought I could get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
## from it.

In my first post I started with the energy conservation equation to get the expression above. However, I think they are independent. Basically, I'm trying to understand how to get ##\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0##, then as you said, I can derive ##
\frac{D}{Dt} \frac{p}{\rho^{\gamma}} = 0
## from it.

I think I understand...
The term ##\nabla P## is 0 for the energy conservation equation and then from there I can get what I'm looking for. Am I correct?
No.
So you accept my two equations?
$$e=\frac{C_Vp}{\rho R}=\frac{p}{\rho}\frac{1}{\gamma-1}\tag{1}$$
and$$\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-p\nabla \centerdot \vec{u}\tag{2}$$If I substitute Eqn. 1 into Eqn.2, I get $$\frac{1}{\gamma-1}\left[\frac{\partial p}{\partial t}+\nabla\centerdot (p \vec{u})\right]=-p\nabla \centerdot \vec{u}\tag{3}$$OK so far?
 
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  • #10
Ah yeah I see. I don't understand why it takes me so long to understand.

Thank you!
 
  • #11
happyparticle said:
Ah yeah I see. I don't understand why it takes me so long to understand.

Thank you!
So we don’t need to show the rest, right?
 
  • #12
Chestermiller said:
So we don’t need to show the rest, right?
No, I'm fine. Thank you.
 
  • #13
I don't know if it's too late, but I realized something.

To get ##
\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
##

I have to use the adiabatic thermal energy balance equation. ##
\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-\nabla(p \vec{u})
##

However, I have to use what you wrote. ##
\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-p\nabla \centerdot \vec{u}\tag{2}
## To get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

Knowing that ##\nabla(p \vec{u}) = p \nabla \cdot \vec{u} + \vec{u} \cdot \nabla p##. It looks like the last term is 0. Why?
 
  • #14
happyparticle said:
I don't know if it's too late, but I realized something.

To get ##
\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
##
Your starting equation is not correct if e is the internal energy per unit mass. The right hand side should be ##-p\nabla \centerdot \vec{u}##. Your first equation does not include the kinetic energy terms. If you include the KE terms, e needs to be replaced by ##e+\frac{1}{2}u^2##, and you need to subtract the velocity vector dotted with the equation of motion.
 
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  • #15
Yet starting from ##
\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-\nabla(p \vec{u})
##

=> ##e[\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{u})] + \rho [ \frac{\partial e}{\partial t} + (\vec{u} \cdot \nabla) e] = -p \nabla \cdot \vec{u} - (\vec{u} \cdot \nabla)p##

The first term on the left hand side is the continuity equation and thus equal to 0.

Thus, using the material derivative I get the expression ##
\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
##

It looks fine to me. However, I couldn't get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##
 
  • #16
happyparticle said:
Yet starting from ##
\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-\nabla(p \vec{u})
##

=> ##e[\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{u})] + \rho [ \frac{\partial e}{\partial t} + (\vec{u} \cdot \nabla) e] = -p \nabla \cdot \vec{u} - (\vec{u} \cdot \nabla)p##

The first term on the left hand side is the continuity equation and thus equal to 0.

Thus, using the material derivative I get the expression ##
\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
##

It looks fine to me. However, I couldn't get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##
The correct equation is
$$\frac{\partial \rho (e+\hat{k})}{\partial t}+\nabla\centerdot (\rho \vec{u}(e+\hat{k}))=-\nabla(p \vec{u})$$
where ##\hat{k}## is the kinetic energy per unit mass: $$\hat{k}=\frac{1}{2}|u|^2$$
In addition, the dot product of the velocity vector with the equation of motion gives the Bernoulli Eqn. $$\rho\frac{D\hat{k}}{Dt}=-\vec{u} \centerdot \nabla p$$
 
  • #17
In the notes I'm following ##\vec{k}## is not taking into account.

Also, With out without ##\vec{k}##, I don't see how to get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0##
 
  • #18
happyparticle said:
In the notes I'm following ##\vec{k}## is not taking into account.

Also, With out without ##\vec{k}##, I don't see how to get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0##
See Transport Phenomena by Bird et al, Chapter 11, large 2-psge-centerfold Table.
 
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  • #19
There are some equations of energy without ##\vec{k}##. Pretty similar that what I'm using. As I said, I can't find a way to get neither of these equations. The whole chapter doesn't mention ##\vec{k}## ##
\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
## or ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

For instance, without ##\vec{k}## I can get ##
\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
## which is something I had to do.

Perhaps I don't express myself well.
 
  • #20
k is the kinetic energy per unit mass. See Eqns. P, Q, and R of BSL Table 11.4.1. Eqn. R is the result of subtracting Eqn. Q from Eqn. P (neglecting viscous stresses and gravitational terms). Note that Eqn. R differs from your energy balance equation, but is of the right form to get your desired results.
 
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  • #21
I'm so confuse. How do you get ##
\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-p\nabla \centerdot \vec{u}\tag{2}
##

The term ## \nabla (-p \vec{u})## in ##
\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-\nabla(p \vec{u})


## come from ##\frac{\Delta W}{ \Delta t}## which is the work against the pressure.

## \frac{\Delta W}{ \Delta t} = \int (-p \hat{n}) \cdot \vec{u} ds##
 
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  • #22
Chestermiller said:
k is the kinetic energy per unit mass. See Eqns. P, Q, and R of BSL Table 11.4.1. Eqn. R is the result of subtracting Eqn. Q from Eqn. P (neglecting viscous stresses and gravitational terms). Note that Eqn. R differs from your energy balance equation, but is of the right form to get your desired results.
Do you agree with equations P and Q?
 
  • #23
Chestermiller said:
Do you agree with equations P and Q?
Yes, if the energy is ##\vec{K} + \vec{U}##
 
  • #24
happyparticle said:
Yes, if the energy is ##\vec{K} + \vec{U}##
Aside from potential energy, that is what it is.
 
  • #25
Why exactly in this case ##e## needs to be replaced by ##
e+\frac{1}{2}u^2
##?
That is what I don't understand.

My initial question was how to get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

Also, I have a similar issue using the Eqn. R. Since Two terms on the right hand side must be 0 to have ##
\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-p\nabla \centerdot \vec{u}\tag{2}


##. Similar to my equation. However, I'm not sure to understand the notation used in the book. At the end of the day, it seems like ##- (\nabla \cdot q) - (\tau; \nabla v) = \vec{u} \cdot \nabla p = 0##
 
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  • #26
happyparticle said:
Why exactly in this case ##e## needs to be replaced by ##
e+\frac{1}{2}u^2
##?
That is what I don't understand.
The total energy of the fluid particles is the sum of internal energy, kinetic energy.
happyparticle said:
My initial question was how to get ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

Also, I have a similar issue using the Eqn. R. Since Two terms on the right hand side must be 0 to have ##
\frac{\partial \rho e}{\partial t}+\nabla\centerdot (\rho \vec{u}e)=-p\nabla \centerdot \vec{u}\tag{2}


##. Similar to my equation. However, I'm not sure to understand the notation used in the book. At the end of the day, it seems like ##- (\nabla \cdot q) - (\tau; \nabla v) = \vec{u} \cdot \nabla p = 0##
The flow is assumed adiabatic, so q = 0. The flow is also assumed inviscid, so the term involving tau is zero. ##\vec{u} \cdot \nabla p## is not assumed to be zero. That term cancels when equations P and Q are combined.
 
  • #27
I see. So basically, my energy balance equation was wrong all along or it was just correct to get ##
\frac{De}{Dt} + (\gamma - 1)e \nabla \cdot \vec{u} = - \frac{1}{\rho} (\vec{u} \cdot \nabla)p
## ?
 
  • #28
happyparticle said:
I see. So basically, my energy balance equation was wrong all along

Yes
 
  • #29
All right.

One more quick question.

To get ##
\frac{D}{Dt} \frac{p}{\rho^{\gamma}} = 0
##

Is it correct to start from ##
\frac{1}{\gamma p} \frac{Dp}{Dt} + \nabla\cdot \vec{u} =
\frac{1}{\rho}[ \frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{u})]
##

Since ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

##
\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{u}) = 0.


##
 
  • #30
happyparticle said:
All right.

One more quick question.

To get ##
\frac{D}{Dt} \frac{p}{\rho^{\gamma}} = 0
##

Is it correct to start from ##
\frac{1}{\gamma p} \frac{Dp}{Dt} + \nabla\cdot \vec{u} =
\frac{1}{\rho}[ \frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{u})]
##

Since ##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0
##

##
\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{u}) = 0.


##
The starting point has to be the energy equation and the mass balance equation, also known as continuity equation.
 
  • #31
Chestermiller said:
This equation is the expression for adiabatic reversible expansion or compression of an ideal gas.

This can be derived from the previous equation using the continuity equation.
I though I had to start with##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0

##
The starting point has to be the energy equation and the mass balance equation, also known as continuity equation.
Basically, I have to do what @pasmith says in post #2?
 
  • #32
happyparticle said:
I though I had to start with##
\frac{Dp}{Dt} + \gamma p \nabla\cdot \vec{u} = 0

##
I don’t think so. This equation can be derived.
 
  • #33
Chestermiller said:
I don’t think so. This equation can be derived.
I guess I misread post #3

I guess I finally found both expression. I think I was completely wrong since the beginning. More than I thought.
 
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FAQ: Different forms of fluid energy conservation equations

What are the different forms of fluid energy conservation equations?

The different forms of fluid energy conservation equations include the Bernoulli equation, the energy equation for compressible and incompressible flows, and the first law of thermodynamics applied to fluid systems. Each of these equations accounts for the conservation of energy in a fluid system, considering various forms of energy such as kinetic, potential, and internal energy.

How is the Bernoulli equation derived?

The Bernoulli equation is derived from the conservation of mechanical energy principle for an ideal fluid flowing along a streamline. It is based on the assumption of steady, incompressible flow with no friction. By applying the work-energy principle and integrating the forces acting on the fluid element, the relationship between pressure, velocity, and elevation is obtained, resulting in the Bernoulli equation.

What assumptions are made in fluid energy conservation equations?

Common assumptions in fluid energy conservation equations include the fluid being incompressible, steady flow conditions, negligible viscosity (ideal fluid), and the absence of energy losses due to friction or turbulence. These assumptions simplify the equations and make them easier to analyze, although they may limit applicability to real-world scenarios.

How do energy losses affect fluid energy conservation equations?

Energy losses, such as those due to friction, turbulence, and heat transfer, affect fluid energy conservation equations by introducing additional terms that account for these losses. In practical applications, the energy equation may include head loss terms (e.g., Darcy-Weisbach or Hazen-Williams equations) to quantify the energy dissipated in the system, which modifies the ideal energy conservation equations.

What is the significance of the energy equation in engineering applications?

The energy equation is crucial in engineering applications as it allows engineers to analyze and design fluid systems, such as pipelines, pumps, and turbines. By understanding energy conservation in fluid flows, engineers can optimize system performance, predict pressure drops, and ensure efficient energy use, making it an essential tool in fluid mechanics and hydraulic engineering.

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