updates, airfoils test
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@@ -5,3 +5,50 @@ Using the equations now, but no numerical methods!
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Still interesting, leverages analytic derivatives of NNs, but lots of problems
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---
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Some notation from SoL:
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The following PDEs typically work with a continuous
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velocity field $\mathbf{u}$ with $d$ dimensions and components, i.e.,
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$\mathbf{u}(\mathbf{x},t): \mathbb{R}^d \rightarrow \mathbb{R}^d $.
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For discretized versions below, $d_{i,j}$ will denote the dimensionality
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of a field such as the velocity,
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with domain size $d_{x},d_{y},d_{z}$ for source and reference in 3D.
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% with $i \in \{s,r\}$ denoting source/inference manifold and reference manifold, respectively.
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%This yields $\vc{} \in \mathbb{R}^{d \times d_{s,x} \times d_{s,y} \times d_{s,z} }$ and $\vr{} \in \mathbb{R}^{d \times d_{r,x} \times d_{r,y} \times d_{r,z} }$
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%Typically, $d_{r,i} > d_{s,i}$ and $d_{z}=1$ for $d=2$.
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For all PDEs, we use non-dimensional parametrizations as outlined below,
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and the components of the velocity vector are typically denoted by $x,y,z$ subscripts, i.e.,
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$\mathbf{u} = (u_x,u_y,u_z)^T$ for $d=3$.
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Burgers' equation in 2D. It represents a well-studied advection-diffusion PDE:
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$\frac{\partial u_x}{\partial{t}} + \mathbf{u} \cdot \nabla u_x =
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\nu \nabla\cdot \nabla u_x + g_x(t),
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\\
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\frac{\partial u_y}{\partial{t}} + \mathbf{u} \cdot \nabla u_y =
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\nu \nabla\cdot \nabla u_y + g_y(t)
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$,
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where $\nu$ and $\mathbf{g}$ denote diffusion constant and external forces, respectively.
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Burgers' equation in 1D without forces with $u_x = u$:
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%\begin{eqnarray}
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$\frac{\partial u}{\partial{t}} + u \nabla u = \nu \nabla \cdot \nabla u $ .
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---
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Later on, Navier-Stokes, in 2D:
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$
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\frac{\partial u_x}{\partial{t}} + \mathbf{u} \cdot \nabla u_x =
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- \frac{1}{\rho}\nabla{p} + \nu \nabla\cdot \nabla u_x \\
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\frac{\partial u_y}{\partial{t}} + \mathbf{u} \cdot \nabla u_y =
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- \frac{1}{\rho}\nabla{p} + \nu \nabla\cdot \nabla u_y \\
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\text{subject to} \quad \nabla \cdot \mathbf{u} = 0,
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$
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