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Lecture notes on the topic of fluid dynamics, specifically focusing on the behavior of a geothermal plume in a porous medium. The notes cover the momentum and energy equations, boundary layer approximation, normalization, and similarity solution. The document also includes equations and their derivations, as well as boundary conditions and computed results.
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Lecture Notes on Fluid Dynamics (1.63J/2.21J) by Chiang C. Mei, 2002
6-5g-plume-L.tex May 11, 2003
R..A.Wooding, (1963), J Fluid Mech. 15, 527-544. C. S. Yih, (1965), Dynamics of Nonhomogeneous Fluids, Macmillan. D. A. Nield and A. Bejan, (1992), Convection in Porous Media. Springer-Verlag. Consider a steady, two dimensional plume due to a source of intense heat in a porous medium. From Darcy’s law: μ k
u = −
∂p ∂x
where k denotes the permeability, and
μ k
w = −
∂p ∂z
− ρg (6.5.2)
These are the momentum equations for slow motion in porous medium. Mass conservation requires ux + wz = 0 (6.5.3)
Energy conservation requires
u
∂x
∂z
= α
∂x^2
∂z^2
where
α =
ρ 0 C
denotes the thermal difusivity. Equation of state: ρ = ρ 0 (1 − β(T − T 0 )) (6.5.6) Consider th flow induced by a strong heat source. Let
T − T 0 = T ′, p = po + p′
where p 0 is the hydrostatic pressure satisfying
−
∂p 0 ∂z
− ρ 0 g = 0.
Eqn. (6.5.2) can be written μ k
w = −
∂p′ ∂z
Eliminating p′^ from Eqns. (6.5.7) and (6.5.1), we get
μ k
(wx − uz) = gρ 0 βT (^) x′.
Let ψ be the stream funciton such that
u = ψz , w = −ψx
then
ψxx + ψzz = −
gρ 0 βk μ
T (^) x′ (6.5.8)
For an intense heat source, we expect the plume to be narrow and tall. Let us apply the boundary layer approximation and check its realm of validity later,
u w,
∂x
∂z
hence
ψxx ∼= −
ρ 0 βk μ
T (^) x′
or
ψx ∼= −
gρ 0 βk μ
which is the same as ignoring ∂p′/∂z in Eqn. (6.5.7). This can be confirmed since u w ∂p′/∂x ≈ 0, p′^ inside the plume is the same as that outside the plume. But ∂p′ ∂z
outside the plume, hence ∂p′/∂z ≈ 0 inside as well. Applying the B.L. approximation to Eqn. (6.5.4)
uT (^) x′ + wT (^) z′ = αT (^) xx′ (6.5.10)
Using the continuity equation we get
(uT ′)x + (wT ′)z = αT (^) xx′.
Integrating across the plume, ∂ ∂z
−∞
wT ′^ dx = 0 (6.5.11)
since T ′^ = 0 outside the plume. It follows that
ρoC
−∞
wT ′^ dx = −ρ 0 C
−∞
ψx T ′^ dx = Q = constant. (6.5.12)
Now let x = λax∗^ z = λbz∗^ ψ = λcψ∗^ θ = λdθ∗.
From Eqn. (6.5.17)
λc−a
∂ψ∗ ∂x∗
= −λdθ∗.
For invariance we require, c − a = d. (6.5.22)
From (6.5.19)
−
∂ψ∗ ∂x∗^
dx∗^ λc−a+a+d^ = 1.
therefore, a + d = 0. (6.5.23)
From Eqn. (6.5.18) λc+d−a−b^ = λd−^2 a.
implying, c + a − b = 0. (6.5.24)
Finally
c =
a 2
, d = −
a 2
, b =
a.
In view of these we introduce the following similarity variables,
η =
x z^2 /^3
, ψ = z^1 /^3 f (η), θ = z−^1 /^3 h(η). (6.5.25)
Note that at the center line η = 0
w = −ψx ∝ z^1 /^3 f ′(0)(−)z−^2 /^3 ∼ z−^1 /^3 f ′(0) ∼ z−^1 /^3 (6.5.26)
θ ∝ z−^1 /^3 h(0) (6.5.27)
and b ∝ z^2 /^3 (6.5.28)
Thus the velocity and temperature along the centerline decay as z−^1 /^3 and the plume width grows as z^2 /^3. Substituting these into Eqns. (6.5.17) and (6.5.18), we get, after some algebra
df dη
= h (6.5.29)
and d dη
(f h) = 3
d^2 h dη^2
The boundary conditions are,
f = 0 (ψ = 0) f ′′(0) = 0 , (w(0, z) = wmax) f (±∞), f ′(±∞) = 0 h(±∞) = 0.
Integrating Eqn. (6.5.30), we get
f h = 3h′.
Using Eqn. (6.5.29), we get f f ′^ = 3f ′′.
Integrating again, we get − 6 f ′^ = f 02 − f 2
where f 0 = fmax. Let f = −f 0 F , then
f 0 (1 − F 2 ) = 6F ′, or
dF 1 − F 2
f 0 dη 6
which can be integrated to give f 0 η 6
ln
Thus (^) ( 1 + F 1 − F
= ef^0 η/^6
or (^) ( 1 + F 1 − F
= ef^0 η/^3
Solving for F , we get
F =
ef^0 /^3 − 1 ef^0 /^3 + 1
= tanh
f 0 η 6
What is f 0? Let us use Eqn. (6.5.29)
−∞
df dη
h dη =
−∞
(f ′)^2 dη = 1
since
f ′^ = −f 0 F ′^ = −
f 02 6
sech^2
f 0 η 6
and h = −f ′.
Figure 6.5.1: Theoretical solution for a geothermal plume due to Yih
From (6.5.36), we get
H B^2
α
α
Qgβ CB
It follows that
H B^3 /^2
α
Qgβ C
Now ψ¯ z ¯^1 /^3
ψ W B
( (^) z H
ψ z^1 /^3
Figure 6.5.2: Comparison of theory and experiment. From Nield and Bejan
It can be shown that
H^1 /^3 W B
Qgβ C
α^1 /^3
Qgβ
which depends on the fluid properties and the given heat source strength. Also z¯^1 /^3 θ = h(η) = (Hz)^1 /^3 ∆T T ” = (H^1 /^3 ∆T )z^1 /^3 T ′^ (6.5.41)
We can show that
ν
gβC
α
Qgβ C
ν(αgβ)^1 /^3 C^2 /^3