diff --git a/modules/openfoam/src/OpenFOAM.f90 b/modules/openfoam/src/OpenFOAM.f90
index 028bc5075..df2619232 100644
--- a/modules/openfoam/src/OpenFOAM.f90
+++ b/modules/openfoam/src/OpenFOAM.f90
@@ -458,7 +458,7 @@ SUBROUTINE SetOpFMForces(p_FAST, u_AD, y_AD, OpFM, ErrStat, ErrMsg)
 #ifdef DEBUG_OPENFOAM
    CALL GetNewUnit( aerodynForcesFile )
    open(unit=aerodynForcesFile,file='fast_aerodyn_velocity_forces.csv')
-   write(aerodynForcesFile,*) '#x, y, z, fx, fy, fz'
+   write(aerodynForcesFile,*) '#x, y, z, u, v, w, fx, fy, fz'
 
    CALL GetNewUnit( actForcesFile )
    open(unit=actForcesFile,file='fast_actuator_forces.csv')
@@ -468,8 +468,8 @@ SUBROUTINE SetOpFMForces(p_FAST, u_AD, y_AD, OpFM, ErrStat, ErrMsg)
    DO K = 1,OpFM%p%NumBl
 
 #ifdef DEBUG_OPENFOAM
-      DO J = 1,u_AD%BladeMotion(k)%NNodes
-        write(aerodynForcesFile,*) u_AD%BladeMotion(k)%TranslationDisp(1,j) + u_AD%BladeMotion(k)%Position(1,j), ', ', u_AD%BladeMotion(k)%TranslationDisp(2,j) + u_AD%BladeMotion(k)%Position(2,j), ', ', u_AD%BladeMotion(k)%TranslationDisp(3,j) + u_AD%BladeMotion(k)%Position(3,j), ', ', OpFM%y%u(1 + (k-1)*u_AD%BladeMotion(k)%NNodes + j), ', ', OpFM%y%v(1 + (k-1)*u_AD%BladeMotion(k)%NNodes + j), ', ', OpFM%y%w(1 + (k-1)*u_AD%BladeMotion(k)%NNodes + j), ', ', y_AD%rotors(1)%BladeLoad(k)%Force(1,j), ', ', y_AD%rotors(1)%BladeLoad(k)%Force(2,j), ', ', y_AD%rotors(1)%BladeLoad(k)%Force(2,j)
+      DO J = 1,u_AD%rotors(1)%BladeMotion(k)%NNodes
+        write(aerodynForcesFile,*) u_AD%rotors(1)%BladeMotion(k)%TranslationDisp(1,j) + u_AD%rotors(1)%BladeMotion(k)%Position(1,j), ', ', u_AD%rotors(1)%BladeMotion(k)%TranslationDisp(2,j) + u_AD%rotors(1)%BladeMotion(k)%Position(2,j), ', ', u_AD%rotors(1)%BladeMotion(k)%TranslationDisp(3,j) + u_AD%rotors(1)%BladeMotion(k)%Position(3,j), ', ', OpFM%y%u(1 + (k-1)*u_AD%rotors(1)%BladeMotion(k)%NNodes + j), ', ', OpFM%y%v(1 + (k-1)*u_AD%rotors(1)%BladeMotion(k)%NNodes + j), ', ', OpFM%y%w(1 + (k-1)*u_AD%rotors(1)%BladeMotion(k)%NNodes + j), ', ', y_AD%rotors(1)%BladeLoad(k)%Force(1,j), ', ', y_AD%rotors(1)%BladeLoad(k)%Force(2,j), ', ', y_AD%rotors(1)%BladeLoad(k)%Force(2,j)
       END DO
 #endif
 
@@ -501,7 +501,7 @@ SUBROUTINE SetOpFMForces(p_FAST, u_AD, y_AD, OpFM, ErrStat, ErrMsg)
       DO K = OpFM%p%NumBl+1,OpFM%p%NMappings
 #ifdef DEBUG_OPENFOAM
       DO J = 1,u_AD%rotors(1)%TowerMotion%NNodes
-         write(aerodynForcesFile,*) u_AD%rotors(1)%TowerMotion%TranslationDisp(1,j) + u_AD%rotors(1)%TowerMotion%Position(1,j), ', ', u_AD%rotors(1)%TowerMotion%TranslationDisp(2,j) + u_AD%rotors(1)%TowerMotion%Position(2,j), ', ', u_AD%TowerMotion%TranslationDisp(3,j) + u_AD%TowerMotion%Position(3,j), ', ', OpFM%y%u(1 + OpFM%p%NumBl*u_AD%BladeMotion(k)%NNodes + j), ', ', OpFM%y%v(1 + OpFM%p%NumBl*u_AD%BladeMotion(k)%NNodes + j), ', ', OpFM%y%w(1 + OpFM%p%NumBl*u_AD%BladeMotion(k)%NNodes + j), ', ', y_AD%rotors(1)%TowerLoad%Force(1,j), ', ', y_AD%rotors(1)%TowerLoad%Force(2,j), ', ', y_AD%rotors(1)%TowerLoad%Force(2,j)
+         write(aerodynForcesFile,*) u_AD%rotors(1)%TowerMotion%TranslationDisp(1,j) + u_AD%rotors(1)%TowerMotion%Position(1,j), ', ', u_AD%rotors(1)%TowerMotion%TranslationDisp(2,j) + u_AD%rotors(1)%TowerMotion%Position(2,j), ', ', u_AD%rotors(1)%TowerMotion%TranslationDisp(3,j) + u_AD%rotors(1)%TowerMotion%Position(3,j), ', ', OpFM%y%u(1 + OpFM%p%NumBl*u_AD%rotors(1)%BladeMotion(k)%NNodes + j), ', ', OpFM%y%v(1 + OpFM%p%NumBl*u_AD%rotors(1)%BladeMotion(k)%NNodes + j), ', ', OpFM%y%w(1 + OpFM%p%NumBl*u_AD%rotors(1)%BladeMotion(k)%NNodes + j), ', ', y_AD%rotors(1)%TowerLoad%Force(1,j), ', ', y_AD%rotors(1)%TowerLoad%Force(2,j), ', ', y_AD%rotors(1)%TowerLoad%Force(2,j)
       END DO
 #endif