link to kutta

seamplex · Jun 15, 2024 · e7a72c5 · e7a72c5
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diff --git a/examples/airfoil.fee b/examples/airfoil.fee
@@ -4,7 +4,7 @@ intro: |
   # Potential flow around an airfoil profile
 
   The Laplace equation can be used to model potential flow.
-  For the particular case of a airfoil profile, the Dirichlet condition at the wing has to satisfy the Kutta condition.
+  For the particular case of a airfoil profile, the Dirichlet condition at the wing has to satisfy the [Kutta condition](https://en.wikipedia.org/wiki/Kutta%E2%80%93Joukowski_theorem).
 
   This example
 

diff --git a/examples/laplace.markdown b/examples/laplace.markdown
@@ -191,7 +191,7 @@ attempt does not seem to be good.</figcaption>
 
 The Laplace equation can be used to model potential flow. For the
 particular case of a airfoil profile, the Dirichlet condition at the
-wing has to satisfy the Kutta condition.
+wing has to satisfy the [Kutta condition].
 
 This example
 
@@ -483,4 +483,5 @@ alt="Potential and velocities zoomed over the airfoil" />
 airfoil</figcaption>
 </figure>
 
+  [Kutta condition]: https://en.wikipedia.org/wiki/Kutta%E2%80%93Joukowski_theorem
   [Joukowsky profile]: https://en.wikipedia.org/wiki/Joukowsky_transform
diff --git a/examples/laplace.md b/examples/laplace.md
@@ -175,7 +175,8 @@ $ ffmpeg -y -framerate 20 -f image2 -i maze-tran-bu-%03d.png maze-tran-bu.gif
 
 The Laplace equation can be used to model potential flow. For the
 particular case of a airfoil profile, the Dirichlet condition at the
-wing has to satisfy the Kutta condition.
+wing has to satisfy the [Kutta
+condition](https://en.wikipedia.org/wiki/Kutta%E2%80%93Joukowski_theorem).
 
 This example