diff --git a/examples/fun3d_examples/ssw_remesh_optimization/README.md b/examples/fun3d_examples/ssw_remesh_optimization/README.md
index 6fc04f91..a594389c 100644
--- a/examples/fun3d_examples/ssw_remesh_optimization/README.md
+++ b/examples/fun3d_examples/ssw_remesh_optimization/README.md
@@ -1,4 +1,4 @@
-# "Super Simple" Wing
+# Simple Subsonic Wing
 Testing out fully-coupled aeroelastic optimizations on a simple wing geometry.
 
 ## Preliminary Sizing
@@ -18,4 +18,4 @@ Twist variable is not used at root station (fixed there)
 Putting it all together
 * 5_shape_and_struct.py - geom twist variables + panel thickness struct variables
 * 6_shape_and_aero.py - geom twist variables + aero aoa variable + airfoil thickness
-* 7_kitchen_sink.py - put all previous variables together : geom twist, airfoil thickness, AOA, panel thickness
\ No newline at end of file
+* 7_kitchen_sink.py - put all previous variables together : geom twist, airfoil thickness, AOA, panel thickness