diff --git a/main.py b/main.py
index 4555fa0..cecc87e 100644
--- a/main.py
+++ b/main.py
@@ -218,7 +218,7 @@ def make_rpm_graph():
 
 if __name__ == '__main__':
     print("Generating RPM Graph")
-    #make_rpm_graph()
+    make_rpm_graph()
     print("Generated")
 
     print("Loading Data & Generating Pressure Graphs")
@@ -318,34 +318,34 @@ if __name__ == '__main__':
             makeGraph(graph, False, figSavePath="./images/pressure/__{0}.png")
 
             
-        if True:
-            aoa = [a[-2] for a in cp_pain_data][1::2]
-            forces = [a[-1] for a in cp_pain_data][1::2]
-            # Force Graphs
-            graph = {
-                    "title":  f"All Total, Lift & Drag Forces\nfor a Clark Y 14% Aerofoil at:\n{raw_data["rpm"]:d}rpm - {raw_data["airSpeed"]:.1f}m/s)", 
-                    "windowTitle": f"All Total, Lift and Drag Forces for a Clark Y 14 Percent Airfoil - {raw_data["rpm"]:d}rpm - {raw_data["airSpeed"]:.1f}m_s",
-                    "xLabel": "Attack Angle [$\\alpha$]", 
-                    "yLabel": "Force [N]",
-                    "grid": True,
-                    "ledgLoc": 1,
-                    "plots": [
-                        {"x":aoa, "y":[f[0] for f in forces], "label":"Total Force"},
-                        {"x":aoa, "y":[f[1] for f in forces], "label":"Lift"},
-                        {"x":aoa, "y":[f[2] for f in forces], "label":"Drag"},
-                    ]
-            }
+    if True:
+        aoa = [a[-2] for a in cp_pain_data][1::2]
+        forces = [a[-1] for a in cp_pain_data][1::2]
+        # Force Graphs
+        graph = {
+                "title":  f"All Total, Lift & Drag Forces\nfor a Clark Y 14% Aerofoil at:\n{raw_data["rpm"]:d}rpm - {raw_data["airSpeed"]:.1f}m/s)", 
+                "windowTitle": f"All Total, Lift and Drag Forces for a Clark Y 14 Percent Airfoil - {raw_data["rpm"]:d}rpm - {raw_data["airSpeed"]:.1f}m_s",
+                "xLabel": "Attack Angle [$\\alpha$]", 
+                "yLabel": "Force [N]",
+                "grid": True,
+                "ledgLoc": 1,
+                "plots": [
+                    {"x":aoa, "y":[f[0] for f in forces], "label":"Total Force"},
+                    {"x":aoa, "y":[f[1] for f in forces], "label":"Lift"},
+                    {"x":aoa, "y":[f[2] for f in forces], "label":"Drag"},
+                ]
+        }
 
-            makeGraph(graph, False, figSavePath="./images/{0}.png", closeFig=True)
+        makeGraph(graph, False, figSavePath="./images/{0}.png", closeFig=True)
 
 
-            print("\n\n")
-            print(raw_data["rpm"])
-            print("AoA         Total    Lift      Drag    ---- Upper Force     Lower Force ")
-            for aoa, force in [(a[-2], a[-1]) for a in cp_pain_data]:
-                print(f"{aoa:d}\\textdegree  & {force[0]:.3f} & {force[1]:.3f} & {force[2]:.3f}  -- {force[4]:.3f}    {force[5]:.3f}     \\\\")
-            print("-"*50)
-            print("\n\n")
+        print("\n\n")
+        print(raw_data["rpm"])
+        print("AoA         Total    Lift      Drag    ---- Upper Force     Lower Force ")
+        for aoa, force in [(a[-2], a[-1]) for a in cp_pain_data]:
+            print(f"{aoa:d}\\textdegree  & {force[0]:.3f} & {force[1]:.3f} & {force[2]:.3f}  -- {force[4]:.3f}    {force[5]:.3f}     \\\\")
+        print("-"*50)
+        print("\n\n")
 
     print("Generating Cp Graphs")