diff --git a/_data/vandv.yml b/_data/vandv.yml
index b2aca204..8a857aae 100644
--- a/_data/vandv.yml
+++ b/_data/vandv.yml
@@ -11,7 +11,8 @@
   - 30p30n
   - swbli
   - LM_transition
-
+  - dsma661
+  
 - title: Incompressible Flow
   vandv:
-  - SANDIA_jet
\ No newline at end of file
+  - SANDIA_jet
diff --git a/_vandv/dsma661.md b/_vandv/dsma661.md
index f3d6ca2a..da6945c9 100644
--- a/_vandv/dsma661.md
+++ b/_vandv/dsma661.md
@@ -1,6 +1,6 @@
 ---
 title: 2D DSMA661 Airfoil Near-Wake RANS Verification Case
-permalink: /vandv/DSMA661/
+permalink: /vandv/dsma661/
 ---
 
 | Solver | Version |
@@ -238,4 +238,4 @@ Additional codes have been compared against the FUN3D and CFL3D results, and are
 <p align="center">
 <img src="/vandv_files/dsma661/images/sst/comp_skinfric_coeff.png" alt="Airfoil Surface Skin Friction Coefficient on Finest Grid">
 </p>
-**Figure (46)**: Airfoil Surface Skin Friction Coefficient on Finest Grid
\ No newline at end of file
+**Figure (46)**: Airfoil Surface Skin Friction Coefficient on Finest Grid
diff --git a/_vandv/index.md b/_vandv/index.md
index 7729f93d..6d1a19fb 100644
--- a/_vandv/index.md
+++ b/_vandv/index.md
@@ -31,7 +31,7 @@ Results for the 30p30n airfoil, mesh independence study at low angle-of-attack,
 Comparison of grid-converged results with experimental data. SA and SST turbulence models.
 * [2D Flat Plate (T3A & T3A-) for Langtry and Menter transition model](/vandv/LM_transition/)
 Comparison of grid-converged results with results of another solver and experimental data.
-* [2D DSMA661 Airfoil Near-Wake RANS Verification Case](/vandv/DSMA661/)
+* [2D DSMA661 Airfoil Near-Wake RANS Verification Case](/vandv/dsma661/)
 Code-to-Code comparisons of grid-converged results of lift, drag and wake profile plots is presented using data from the NASA Turbulence Modeling Resource.