Conservation Laws from Continuity Equations in Fluid Flow

In summary, Frankel's "The Geometry of Physics" discusses how differential forms can be used to generalize Reynolds Transport Theorem. By doing so, it is possible to determine the conservation of mass when considering a flow of fluid. However, this conservation is not always explicit and must be inferred.
  • #1
Stuart_M
2
0
TL;DR Summary
There is a version of Reynolds Transport Theorem for differential forms: what is the conserved quantity?
Consider a fluid flow with density ##\rho=\rho(t,x)## and velocity vector ##v=v(t,x)##. Assume it satisfies the continuity equation
$$
\partial_t \rho + \nabla \cdot (\rho v) = 0.
$$
We now that, by Reynolds Transport Theorem (RTT), this implies that the total mass is conserved
$$
\frac{d}{dt}\int_{\Omega_t} \rho dx = 0,
$$
where ##\Omega_t## is some control volume (which I understand in the following way: I fix a region ##\Omega## at time ##0##; I let ##\Omega## evolve with the flow at time ##t## and I obtain ##\Omega_t=\Phi_t(\Omega)##). I have recently been reading Frankel's "The Geometry of Physics" and I've learnt that using differential forms it is possible to generalise (RTT) in the following way (see Chapter 4, Section 3):
$$
\frac{d}{dt} \int_{S(t)} \alpha = \int_{S(t)} (\partial_t \alpha + L_v \alpha)
$$
where now ##\alpha## are (time-indexed family of) ##p##-forms, ##S## is a fixed ##p##-manifold and ##S(t) = \Phi_t(S)## is the evolution of ##S## under the flow of ##v##, and ##L_v## denotes the Lie derivative. From this we easily deduce that, if a ##p##-form satisfies the "continuity equation"
$$
\partial_t \alpha + L_v \alpha = 0
$$
then the quantity ##\int_{S(t)} \alpha## is constant in time. If ##\alpha## is a (top-dimensional) volume form, then we recover (RTT) and thus the conservation of *mass*. However, in the general case what does the quantity ##\int_{S(t)} \alpha## represent?

I have considered some easy toy examples: if ##\alpha = f## is a ##0##-form (i.e. scalar function), then the "continuity equation" reads ##\partial_t f + v \cdot \nabla f = 0##, whence ##f(t,\Phi_t(x)) = f(0,x)## and indeed this can be expressed as "conservation of the integral of ##f## on 0-dimensional manifolds". However, which quantity is conserved?

Another example [taken from Frankel, ibidem]: in Euler, the vorticity *form* ##\omega=d \nu## (##\nu## being the velocity *co*vector) is invariant under the flow, i.e. solves the continuity equation in the sense of 2-forms. Therefore,
$$
\int_{S(t)} \omega
$$
is constant for any 2-manifold ##S##. Which conservation law am I rediscovering? Which conserved quantity is this?
 
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  • #2
In fluid mechanics, we have transport equations for the following:

Global quantityLocal quantity
MassDensity
MomentumMomentum per unit volume
EnergyEnergy per unit volume
Amount of substanceConcentration
(No standard name)Vorticity
Concentration is either amount per unit mass or amount per unit volume.

Note that [itex]\int \alpha[/itex] is not necessarily conserved itself; it is also necessary to account for sources and sinks of the quantity.
 
  • #3
pasmith said:
In fluid mechanics, we have transport equations for the following:

Global quantityLocal quantity
MassDensity
MomentumMomentum per unit volume
EnergyEnergy per unit volume
Amount of substanceConcentration
(No standard name)Vorticity
Concentration is either amount per unit mass or amount per unit volume.

Note that [itex]\int \alpha[/itex] is not necessarily conserved itself; it is also necessary to account for sources and sinks of the quantity.
Thank you for your reply and for the table.
I am not sure I am able to see the link with my question with differential forms, though. Is there a way to phrase the momentum per unit volume (or the energy per unit volume) as a differential form? If so, can we say that this form satisfies the "continuity equation" (in the right formulation) and deduce the conservation of the corresponding global quantity? But this would seem strange to me: by the generalized RTT we would we get the conservation of this quantity only when "integrated" over some p-dimensional manifold (I'm in an ideal world, no sinks/sources for the time being). What does this mean? Is this some sort of generalized flux? I'm sorry for my confusion, I hope somebody can shed some light here. Thanks!
 

FAQ: Conservation Laws from Continuity Equations in Fluid Flow

What are conservation laws in the context of fluid flow?

Conservation laws in fluid flow refer to principles that dictate the preservation of certain quantities, such as mass, momentum, and energy, within a fluid system. These laws are derived from fundamental physical principles and are expressed mathematically through continuity equations. They ensure that the total amount of these conserved quantities remains constant over time, barring any external influences.

What is the continuity equation for mass conservation?

The continuity equation for mass conservation states that the mass of fluid entering a control volume must equal the mass of fluid leaving the control volume, plus any accumulation of mass within the control volume. Mathematically, it is expressed as ∂ρ/∂t + ∇·(ρv) = 0, where ρ is the fluid density, t is time, and v is the velocity vector of the fluid.

How is momentum conservation applied in fluid dynamics?

Momentum conservation in fluid dynamics is described by the Navier-Stokes equations. These equations account for the forces acting on a fluid element, including pressure, viscous, and external forces. The general form is ρ(∂v/∂t + v·∇v) = -∇p + μ∇²v + ρg, where ρ is the fluid density, v is the velocity vector, p is the pressure, μ is the dynamic viscosity, and g is the gravitational acceleration vector.

What role does energy conservation play in fluid flow analysis?

Energy conservation in fluid flow is governed by the first law of thermodynamics, which states that the total energy within a control volume must remain constant, accounting for energy entering and leaving the system, as well as any work done and heat transferred. The energy equation can be represented as ρ(∂e/∂t + v·∇e) = -∇·q + Φ, where e is the specific energy, q is the heat flux, and Φ is the dissipation function due to viscous effects.

How are continuity equations derived from conservation laws?

Continuity equations are derived from conservation laws by applying the principles of mass, momentum, and energy conservation to an infinitesimally small control volume within the fluid. By considering the flux of these conserved quantities across the boundaries of the control volume and applying the divergence theorem, the differential forms of the continuity equations are obtained, which describe the local behavior of the fluid.

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