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Modern Engineering Thermodynamics

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19.5 Thermomechanical Coupling 777<br />

Under isothermal conditions (dT = 0), Eq. (19.34) gives<br />

<br />

J T¼constant Q = − vL <br />

QM dp<br />

T dx<br />

This equation describes the mechanocaloric effect, which is usually modeled after Fourier’s law as<br />

<br />

<br />

J T¼constant<br />

dp<br />

Q = − k o<br />

dx<br />

(19.36)<br />

(19.37)<br />

where k o is an empirical material constant called the osmotic heat conductivity coefficient. Comparing Eqs. (19.36)<br />

and (19.37), using Onsager’s reciprocity relation and ρ = 1/v, we see that<br />

L QM = Tk o /v = ρTk o = L MQ (19.38)<br />

Similarly, the mass flux under isothermal conditions (dT = 0) is given by Eq. (19.35) as<br />

<br />

J T¼constant M = vL <br />

MM dp<br />

T dx<br />

(19.39)<br />

Now, two flow models can be used to interpret this equation. The first was formulated empirically in 1856 by<br />

the French hydraulic engineer Henri Philibert Gaspard Darcy (1803–1858) for flow through porous media.<br />

Appropriately called Darcy’s law, it states that the bulk fluid velocity in a porous material is given by<br />

V = − k p<br />

μ<br />

<br />

<br />

dp<br />

dx<br />

(19.40)<br />

where μ is the fluid viscosity and k p is called the permeability of the porous material. 13 Comparing Eqs. (19.39)<br />

and (19.40) and introducing the mass flux definition along with the relation ρ = 1/v produces<br />

<br />

J T¼constant M = ρV = − ρk <br />

p dp<br />

= − vL <br />

MM dp<br />

(19.41)<br />

μ dx T dx<br />

from which it is clear that the mass flow primary coefficient L MM is<br />

L MM = ρ 2 Tk p /μ (19.42)<br />

The other flow model that can be used in Eq. (19.39) was developed for flow through a circular tube and<br />

is called the Darcy-Weisbach equation after Henri Darcy and the German engineer Julius Ludwig Weisbach<br />

(1806–1871). In this model, the isothermal mass flux is given by<br />

<br />

J T M =constant<br />

= ρV = − 2Dg <br />

c dp<br />

(19.43)<br />

fV dx<br />

where D is the tube diameter and f is an empirically determined “friction factor.” The value of f can be found<br />

in most fluid mechanics textbooks from a generalized curve of f versus the dimensionless Reynolds number,<br />

ρVD/μ. It can be shown that, if the flow is laminar (ρVD/μ < 2000), then<br />

J M<br />

<br />

T¼constant = ρV = − ρD2<br />

32μ<br />

<br />

<br />

dp<br />

dx<br />

(19.44)<br />

By comparing Eqs. (19.41) and (19.44), we see that these equations are similar and they become identical when<br />

we define the effective permeability of a circular tube as<br />

Thus, for very slow flow through a circular tube, we can write<br />

k p = D 2 /32 (19.45)<br />

L MM = TðρDÞ2<br />

(19.46)<br />

32μ<br />

Finally, combining Eqs. (19.34) and (19.35) to eliminate the term (v/T)(dp/dx) gives<br />

<br />

J Q = − L 2<br />

<br />

QQL MM − L QM dp<br />

L MM T 2<br />

− L QM<br />

dx T J M (19.47)<br />

13 The common unit of measure of permeability is the darcy, which has the rather awkward definition of 1 darcy being the<br />

permeability that allows the flow of 1 cm 3 /s of fluid with a pressure gradient of 1 atm/cm. The darcy is not an SI unit. The SI unit for<br />

permeability is m 2 , where 1 darcy = 10 −12 m 2 .

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