Rayleigh-Bénard
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One of the widely studied instabilities is the so-called Rayleigh Bernard instability that describes the structure of cells that forms when a liquid enters convection in a temperature gradient.
ID:(1168, 0)
Rayleigh-Bénard
Description
One of the widely studied instabilities is the so-called Rayleigh Bernard instability that describes the structure of cells that forms when a liquid enters convection in a temperature gradient.
Variables
Calculations
Calculations
Equations
(ID 9218)
(ID 9219)
Examples
When a liquid in a gravitational field with acceleration $g$ is exposed to two horizontal plates with upper temperature $T_t$ and lower temperature $T_b$, where the lower temperature is greater than the upper temperature, a spontaneous flow is generated if the Rayleigh number
| $R_c=\displaystyle\frac{g\alpha}{d\nu}(T_b-T_t)L^3$ |
exceeds a critical value. In this case, $L$ represents the distance between the plates, $d$ is the diffusivity, $\alpha$ is the thermal expansion coefficient, and $
u$ is the kinematic viscosity.
You can find more information at this link: http://home.iitk.ac.in/~sghorai/NOTES/benard/benard.html
(ID 9216)
The eigenvalue problem becomes
$(D^2-a^2)^3W=-a^2R_aW$
subject to the boundary condition
$W=D^2W=D^4W=0 at
From this, we can show that
$D^{2m}W=0$
for
$z=0,1$
and
$m = 1,2,\cdots$
It follows that the required solution must be
$W=A\sin(n\pi z)$
with
$n=1,2,3,\cdots$
where A is a constant and n is an integer. Substituting W leads to the eigenvalue relationship
$R_a=\frac{(n^2\pi^2+a^2)^3}{a^2}$
For a given
$a^2$
, the lowest value of
$R_c$
occurs when
$n=1$
which is the lowest mode:
$R_a=\frac{(\pi^2+a^2)^3}{a^2}$
The critical Rayleigh number
$R_c$
is obtained by finding the minimum value of
$R_a$
as
$a^2$
varies.
$\frac{dR_a}{da^2}=0\rightarrow a_c=\frac{\pi}{\sqrt{2}}$
and the corresponding
$R_c$
is given by
| $R_c=\displaystyle\frac{27}{4}\pi^4$ |
(ID 9217)
If we set the origin at the midpoint of the chamber, the problem to be solved is given by
$(D^2-a^2)^3W=-a^2R_aW$
subject to the boundary condition
$W=DW=(D^2-a^2)^2W=0$
at
$z=0,1$
.
The problem is symmetric with respect to the two boundaries, so the eigenfunctions are divided into two distinct classes: (even mode), which has vertical velocity symmetry with respect to the midplane, and (odd mode), which has vertical velocity antisymmetry. The even mode has a single row of cells along the vertical, while the odd mode has two rows of cells. Let\'s assume the solution is of the form
$W=e^{qz}$
where the roots $q$ are given by
$(q^2-a^2)^3=-R_a^2$
Let
$R_a^2=\lambda^3a^6$
then the roots are given by
$q^2=-a^2(\lambda-1)$
and
$q^2=a^2\left[1+\frac{1}{2}\frac{\sqrt{3}}{2}\right]$
Taking the square root again, the roots are $\pm iq_0$, $\pm q$, and $\pm q^*$, where $q_0=a\sqrt{\lambda-1}$ and
$re(q)=q_1=a\left[\frac{1}{2}\sqrt{1+\lambda+\lambda^2}+\frac{1}{2}\sqrt{1+\frac{\lambda}{2}}\right]^{1/2}$
$im(q)=q_2=a\left[\frac{1}{2}\sqrt{1+\lambda+\lambda^2}-\frac{1}{2}\sqrt{1+\frac{\lambda}{2}}\right]^{1/2}$
Here, $q^*$ denotes the complex conjugate of $q$. From these relationships, we have
$(q_0^2+a^2)^2=a^4\lambda^2$
$(q^2-a^2)^2=\frac{1}{2}a^4\lambda^2(-1\pm i\sqrt{3})$
Even mode solution
The even mode solution is expressed as
$W=A\cos(q_0z)+B\cosh(qz)+C\cosh(q^*z)$
Therefore, we have
$DW=-Aq_0\sin(q_0z)+Bq\sinh(qz)+Cq^*\sinh(q^*z)$
$(D^2-a^2)^2W=A(q_0^2+a^2)^2\cos(q_0z)+B(q^2-a^2)+C(q^{*2}-a^2)^2\cosh(q^*z)$
The boundary conditions provide
$\left[\begin{array}{ccc}\cos(q_0/2) & \cosh(q/2) & \cosh(q^/2) \ \sin(q_0/2) & \sinh(q/2) & \sinh(q^/2) \ -q_0\tan(q_0/2) & q\tanh(q/2) & q^\tanh(q^/2)\end{array}\right]\left[\begin{array}{c}A \ B \ C\end{array}\right]=0$
For a nontrivial solution (after some manipulations), we must have
$\displaystyle\left\vert\begin{array}{ccc} 1 & 1 & 1 \ -q_0\tan(q_0/2) & q\tanh(q/2) & q^\tanh(q^/2) \ \frac{1}{2}(i\sqrt{3}+1) & \frac{1}{2}(i\sqrt{3}-1) & -1\end{array}\right\vert=0$
which, in simplified terms,
$im\left[(\sqrt{3}+i)q\tanh(q/2)\right]+q_0\tan(q_0/2)=0$
which can be written as (with further simplification)
$-q_0\tan(q_0/2)=\frac{(q_1+q_2\sqrt{3})\sinh(q_1)+(q_1\sqrt{3}-q_2)\sin(q_2)}{\cosh(q_1)+\cos(q_2)}$
This equation must be solved using the trial and error method: for a given value of $a$, we need to find the value of $\lambda$ and then find the value of $R_a$. The critical values of $a$ and $R_a$ (Reid & Harris, Phys of Fluids, Vol-1) are given by
$a_c=3.117 and
Taking $A_0=1$ and $C=B^*$, we can find $W$ and $\Theta$.
Impar Solution
The odd solution is represented as
$W=A\sin(q_0z)+B\sinh(qz)+C\sinh(q^*z)$
Proceeding similarly, we obtain
$q_0\cot(q_0/2)=\displaystyle\frac{(q_1+q_2\sqrt{3})\sinh(q_1)-(q_1\sqrt{3}-q_2)\sin(q_2)}{\cosh(q_1)-\cosh(q_2)}$
In this case, the minimum Rayleigh number occurs at $a=5.365$, and the corresponding value of the Rayleigh number is
| $R=17610.39$ |
.
(ID 9219)
The solution for the case where the upper surface is free and the lower surface is rigid can be deduced from the odd solution of the rigid-rigid box.
The problem is defined by:
$\frac{(D^2-a^2)^3}{W}=-a^2R_aW$
subject to the boundary condition:
$W = DW = (D^2-a^2)^2W = 0$
at
$z = 0$
$W = D^2W = D^4W = 0$
at
$z = 1$
The boundary conditions at the mid-height for the odd solution hold. Therefore, an odd solution for the rigid-rigid limit at depth
$d$
provides a solution for the rigid-free limit at depth
$d/2$
. Thus, using the stability results from the rigid-rigid case, we have:
$a_c = 5.365 / 2 \approx 2.682$
and
$R_c = 17610.39 / 2^4 \approx 1100.65$
[Note: From the dimensional form of
$\Delta_1^2f + k^2f$
, we have
$a = kL$
(where
$L$
is the scale length) as the dimensionless wavenumber.]
| $$ |
(ID 9218)
ID:(1168, 0)
