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Merge pull request #31 from S-Explorer/development
fix introduction sample case typo
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Docs/IAMReX_documentation/source/Introduction_Chapter.rst

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@@ -18,7 +18,7 @@ Key software and algorithmic features of IAMR include:
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Sample Cases
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------------------
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In the first case, we test the order of convergence for in a 2D reversed single vortex problem.
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In the first case, we test the order of convergence for in a 2D reversed single vortex problem.
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A 2D circular drop with radius R=0.15 is placed at (0.5,0.75) in a unit computational domain [0, 1] x [0, 1].
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The velocity field is given by the stream function,
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\Psi(x, y, t)=\frac{1}{\pi} \sin ^{2}(\pi x) \sin ^{2}(\pi y) \cos \left(\frac{\pi t}{T}\right),
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in which the rotational period is $T=4.0$. The velocities in the $x$ and $y$ directions are defined as $u(x,y,t)=\partial \Psi / \partial y$ and $v(x,y,t)=-\partial \Psi / \partial x$, respectively.
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The periodic boundary condition is applied in both x and y directions. At t=T, the interfacial profile of the drop at the high resolution converges to its initial profile, which represents the exact solution.
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in which the rotational period is :math:`T=4.0`. The velocities in the :math:`x` and :math:`y` directions are defined as :math:`u(x,y,t)=\partial \Psi / \partial y` and :math:`v(x,y,t)=-\partial \Psi / \partial x`, respectively.
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The periodic boundary condition is applied in both x and y directions. At t=T, the interfacial profile of the drop at the high resolution converges to its initial profile, which represents the exact solution.
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On the other hand, the circular shape of the drop is distorted for the simulation with low resolution.
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Here is the case directory: `RSV <https://github.com/ruohai0925/IAMReX/tree/development/Tutorials/RSV>`_.
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Profiles of drop interface in the Reverse Single Vortex (RSV) problem at t/T=1 after one rotation. Black line: Analytical Solution; Red line: 64*64; Blue line: 128*128; Green line: 256*256
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The second Rayleigh--Taylor (RT) instability case is simulated here to validate the adaptive two-phase flow algorithms when small vorticity structures are involved.
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This instability phenomenon occurs for any perturbation to the interface between a lighter fluid ($\rho_2$) at the bottom and a heavier fluid ($\rho_1$) at the top.
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In the simulation, the computational domain is $[0,1] \times [0,4]$. The initial interface is given by $y(x)=2.0+0.1\cos(2\pi x)$.
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The density ratio is set to $\lambda=\rho_2/\rho_1=1/3$ and the Reynolds number is set to be $Re=\rho_1 g^{1/2}/\mu_1=3000$. Here is the case directory: `RayleighTaylor <https://github.com/ruohai0925/IAMReX/tree/development/Tutorials/RayleighTaylor_LS>`_.
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This instability phenomenon occurs for any perturbation to the interface between a lighter fluid (:math:`\rho_2`) at the bottom and a heavier fluid (:math:`\rho_1`) at the top.
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In the simulation, the computational domain is :math:`[0,1] \times [0,4]`. The initial interface is given by :math:`y(x)=2.0+0.1\cos(2\pi x)`.
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The density ratio is set to :math:`\lambda=\rho_2/\rho_1=1/3` and the Reynolds number is set to be :math:`Re=\rho_1 g^{1/2}/\mu_1=3000`. Here is the case directory: `RayleighTaylor <https://github.com/ruohai0925/IAMReX/tree/development/Tutorials/RayleighTaylor_LS>`_.
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.. figure:: ./GettingStarted/IAMR_LSAMR.png
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:align: center
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Contours of velocity magnitude in yz plane
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All input scripts and raw postprocessing data of IAMReX have been uploaded into `Baidu Cloud <https://pan.baidu.com/s/1bZRoDunjBv7bqYL8CI3ASA?pwd=i5c2>`_ for interested readers to reproduce the results.
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All input scripts and raw postprocessing data of IAMReX have been uploaded into `Baidu Cloud <https://pan.baidu.com/s/1bZRoDunjBv7bqYL8CI3ASA?pwd=i5c2>`_ for interested readers to reproduce the results.

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