Conservation of Mass for Compressible Flow

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SUMMARY

The discussion focuses on the application of the conservation of mass principle in compressible flow, particularly in a system involving a piston pushing air through a tube. The key equations presented include the mass inside the control volume, expressed as $$ M_{cv} = \int_0^{u(t)} A~ \rho (u,t)~du $$, and the rate of change of mass, $$ \frac{d}{dt}M_{cv} = - A \rho_o(t) v_o(t) $$. Participants emphasize the need for additional equations, such as conservation of momentum and an equation of state, to fully solve for the density function $$ \rho(u,t) $$ and velocity $$ v(u,t) $$, as the current setup lacks sufficient information to derive these variables independently.

PREREQUISITES
  • Understanding of compressible flow dynamics
  • Familiarity with partial differential equations
  • Knowledge of conservation laws in fluid mechanics
  • Basic principles of control volume analysis
NEXT STEPS
  • Study the Navier-Stokes equations for compressible flow
  • Learn about the derivation of the continuity equation in fluid dynamics
  • Explore the application of equations of state in compressible flow scenarios
  • Investigate the effects of viscosity on pressure gradients in fluid systems
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Fluid mechanics students, engineers working with compressible flow systems, and researchers interested in the mathematical modeling of fluid dynamics will benefit from this discussion.

  • #31
wrobel said:
Let ##\omega## be a k-form on m-dimensional manifold ##M,\quad m\ge k.## Let ## v## be a vector field on ##M## and ##g^t## be its flow.

Let ##S\subset M## be a k-dimensional compact submanifold. Then
$$\frac{d}{dt}\Big|_{t=0}\int_{g^t(S)}\omega=\int_SL_v\omega.$$ Here ##L_v## is a Lie derivative and the formula follows directly from the change of variables.

Particularly if k=m then ##\omega=\rho(x)dx^1\wedge\ldots\wedge dx^m## and
$$L_v\omega=\frac{\partial (\rho v^i)}{\partial x^i} dx^1\wedge\ldots\wedge dx^m.$$

From the group property it is not hard to show that the following conditions are equivalent

1) ##\frac{d}{dt}\Big|_{t=0}\int_{g^t(S)}\omega=0## for any k-dimensional compact submanifold S;
2) ##\frac{d}{dt}\int_{g^t(S)}\omega=0,\quad \forall t## and for any k-dimensional compact submanifold S;
3) ##L_v\omega=0##

This method is covering a lot of different circulations theorems in electrodynamics and hydro dynamics as well
In the fluid-mechanics literature those are known also as "Reynolds transport theorems". This is the modern Cartan-calculus formulation of them.
 
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  • #32
Yes! Elie Cartan's integral invariants.

Df. A form ##\omega## is called relative integral invariant iff ##L_v\omega=d\Omega\quad (\exists \Omega)##.
A form ##\alpha## is called absolute integral invariant iff ##L_v\alpha=0##.

If ##\omega## is a relative integral invariant then ##d\omega## is an absolute integral invariant: ##L_vd\omega=dL_v\omega=dd\Omega##
and
$$\frac{d}{dt}\Big|_{t=0}\int_{g^t(S)}\omega=\int_SL_v\omega=\int_{\partial S}\Omega.$$

For further play with these formulas use
$$L_v\omega=i_vd\omega+di_v\omega;$$

De Rham's theorem is also near here
etc.

For example in the extended phase space of a Hamiltonian system one has: ##dp_i\wedge dx^i-dH\wedge dt## is an absolute integral invariant; ##p_idx^i-Hdt## is a relative integral invariant.
 
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  • #33
vanhees71 said:
In the fluid-mechanics literature those are known also as "Reynolds transport theorems". This is the modern Cartan-calculus formulation of them.
The funny thing is, I know about Reynolds Transport Theorems, but I never would have recognized that(and frankly still can’t)! @wrobel said “k form on m dimensional manifold” and my head exploded. 🤯
 
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  • #34
The advantage of the modern Cartan calculus is that it becomes in a way very natural, and it's very general too, because it works not only in (pseudo)-Riemannian manifolds but in general differentiable manifolds, i.e., the Lie derivative and Stokes's theorem for alternating (differential) forms are independent of any additional structures like connections and/or (pseudo-)metrics.
 
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