diff --git a/docs/src/literate/C_customizablePreprocessing.jl b/docs/src/literate/C_customizablePreprocessing.jl
index 05aa24fa..acfee8aa 100644
--- a/docs/src/literate/C_customizablePreprocessing.jl
+++ b/docs/src/literate/C_customizablePreprocessing.jl
@@ -22,7 +22,7 @@ import PyPlot
 import OWENSOpenFASTWrappers
  
 
-path = runpath = "/home/runner/work/OWENS.jl/OWENS.jl/docs/src/literate" #bld_height_numadsplitdir(@__FILE__)[1]
+path = runpath = "/home/runner/work/OWENS.jl/OWENS.jl/docs/src/literate" #splitdir(@__FILE__)[1]
 
 Inp = OWENS.MasterInput("$runpath/sampleOWENS.yml")
 
diff --git a/src/Unsteady.jl b/src/Unsteady.jl
index 7093cbce..8d6b9ace 100644
--- a/src/Unsteady.jl
+++ b/src/Unsteady.jl
@@ -384,7 +384,7 @@ function Unsteady(inputs;topModel=nothing,topMesh=nothing,topEl=nothing,
                             if inputs.AD15On
                                 aeroVals,aeroDOFs = run_aero_with_deformAD15(aero,deformAero,topMesh,topEl,u_j,udot_j,uddot_j,inputs,t[i],azi_j,Omega_j,OmegaDot_j)
                             else
-                                aeroVals,aeroDOFs = run_aero_with_deform(aero,deformAero,topMesh,topEl,u_j,uddot_j,inputs,numIterations,t[i],azi_j,Omega_j,top_grav_setting)
+                                aeroVals,aeroDOFs = run_aero_with_deform(aero,deformAero,topMesh,topEl,u_j,uddot_j,inputs,numIterations,t[i],azi_j,Omega_j,topModel.gravityOn)
                             end
                         end
                     end
@@ -577,7 +577,7 @@ function Unsteady(inputs;topModel=nothing,topMesh=nothing,topEl=nothing,
                                 if inputs.AD15On
                                     aeroVals,aeroDOFs = run_aero_with_deformAD15(aero,deformAero,topMesh,topEl,u_j,udot_j,uddot_j,inputs,t[i],azi_j,Omega_j,OmegaDot_j)
                                 else
-                                    aeroVals,aeroDOFs = run_aero_with_deform(aero,deformAero,topMesh,topEl,u_j,uddot_j,inputs,numIterations,t[i],azi_j,Omega_j,top_grav_setting)
+                                    aeroVals,aeroDOFs = run_aero_with_deform(aero,deformAero,topMesh,topEl,u_j,uddot_j,inputs,numIterations,t[i],azi_j,Omega_j,topModel.gravityOn)
                                 end
                             end
                         end
diff --git a/src/utilities.jl b/src/utilities.jl
index b514b05d..8402bf26 100644
--- a/src/utilities.jl
+++ b/src/utilities.jl
@@ -330,7 +330,7 @@ function owens(owensfile,analysisType;
 
         aeroForces(t,azi) = externalForcing(t+delta_t,aerotimeArray,aeroForceValHist,aeroForceDof)
 
-        deformAero(azi;newOmega=-1,newVinf=-1,bld_x=-1,bld_z=-1,bld_twist=-1) = 0.0 #placeholder function
+        deformAero(azi;newOmega=-1,newVinf=-1,bld_x=-1,bld_z=-1,bld_twist=-1,accel_flap_in=-1,accel_edge_in=-1,gravity=-1) = 0.0 #placeholder function
         Unsteady(model;topModel=feamodel,topMesh=mesh,topEl=el,bin,aero=aeroForces,deformAero)
 
         return model
diff --git a/test/34mROMtest.jl b/test/34mROMtest.jl
index 0240af6c..570b0eae 100644
--- a/test/34mROMtest.jl
+++ b/test/34mROMtest.jl
@@ -33,7 +33,7 @@ for i=1:length(myel2["props"])
 end
 myel = OWENSFEA.El(sectionPropsArray,myel2["elLen"],myel2["psi"],myel2["theta"],myel2["roll"],myel2["rotationalEffects"])
 
-deformTurb2(a;newOmega=-1,newVinf=-1, bld_x=-1, bld_z=-1, bld_twist=-1) = 0
+deformTurb2(a;newOmega=-1,newVinf=-1, bld_x=-1, bld_z=-1, bld_twist=-1,accel_flap_in=-1,accel_edge_in=-1,gravity=-1) = 0
 
 delta_t = 0.1
 function aeroForcesDMS(t,azi)