Fix clumsy find-replace

ferram4 · May 22, 2017 · dcbc1ac · dcbc1ac
1 parent 026d8ff
commit dcbc1ac
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Showing 4 changed files with 8 additions and 8 deletions.
diff --git a/FerramAerospaceResearch/FARAeroComponents/FARAeroSection.cs b/FerramAerospaceResearch/FARAeroComponents/FARAeroSection.cs
@@ -284,7 +284,7 @@ public void ClearAeroSection()
             handledAeroModulesIndexDict.Clear();
         }
 
-        public void PredictionCalculateAeroForces(float atmDensity, float machNumber, float reynoldsPerUnitLength, float pseudode LavalNumber, float skinFrictionDrag, Vector3 vel, ferram4.FARCenterQuery center)
+        public void PredictionCalculateAeroForces(float atmDensity, float machNumber, float reynoldsPerUnitLength, float pseudoKnudsenNumber, float skinFrictionDrag, Vector3 vel, ferram4.FARCenterQuery center)
         {
             if (partData.Count == 0)
                 return;
@@ -351,7 +351,7 @@ public void PredictionCalculateAeroForces(float atmDensity, float machNumber, fl
             nForce *= normalForceFactor;
 
             double xForce = -skinFrictionForce * Math.Sign(cosAoA) * cosSqrAoA;
-            double localVelForce = xForce * pseudode LavalNumber;
+            double localVelForce = xForce * pseudoKnudsenNumber;
             xForce -= localVelForce;
 
             localVelForce = Math.Abs(localVelForce);
@@ -430,7 +430,7 @@ public void PredictionCalculateAeroForces(float atmDensity, float machNumber, fl
             center.AddTorque(torqueVector);
         }
 
-        public void FlightCalculateAeroForces(float atmDensity, float machNumber, float reynoldsPerUnitLength, float pseudode LavalNumber, float skinFrictionDrag)
+        public void FlightCalculateAeroForces(float atmDensity, float machNumber, float reynoldsPerUnitLength, float pseudoKnudsenNumber, float skinFrictionDrag)
         {
 
             double skinFrictionForce = skinFrictionDrag * xForceSkinFriction.Evaluate(machNumber);      //this will be the same for each part, so why recalc it multiple times?
@@ -489,7 +489,7 @@ public void FlightCalculateAeroForces(float atmDensity, float machNumber, float
                 nForce *= normalForceFactor;
 
                 double xForce = -skinFrictionForce * Math.Sign(cosAoA) * cosSqrAoA;
-                double localVelForce = xForce * pseudode LavalNumber;
+                double localVelForce = xForce * pseudoKnudsenNumber;
                 xForce -= localVelForce;
 
                 localVelForce = Math.Abs(localVelForce);

diff --git a/FerramAerospaceResearch/FARAeroComponents/FARVesselAero.cs b/FerramAerospaceResearch/FARAeroComponents/FARVesselAero.cs
@@ -271,7 +271,7 @@ private void CalculateAndApplyVesselAeroProperties()
             reynoldsNumber = FARAeroUtil.CalculateReynoldsNumber(vessel.atmDensity, Length, vessel.srfSpeed, machNumber, FlightGlobals.getExternalTemperature((float)vessel.altitude, vessel.mainBody), vessel.mainBody.atmosphereAdiabaticIndex);
             float skinFrictionDragCoefficient = (float)FARAeroUtil.SkinFrictionDrag(reynoldsNumber, machNumber);
 
-            float pseudode LavalNumber = (float)(machNumber / (reynoldsNumber + machNumber));
+            float pseudoKnudsenNumber = (float)(machNumber / (reynoldsNumber + machNumber));
 
             Vector3 frameVel = Krakensbane.GetFrameVelocityV3f();
 
@@ -295,7 +295,7 @@ private void CalculateAndApplyVesselAeroProperties()
                 }*/
 
             for (int i = 0; i < _currentAeroSections.Count; i++)
-                _currentAeroSections[i].FlightCalculateAeroForces(atmDensity, (float)machNumber, (float)(reynoldsNumber / Length), pseudode LavalNumber, skinFrictionDragCoefficient);
+                _currentAeroSections[i].FlightCalculateAeroForces(atmDensity, (float)machNumber, (float)(reynoldsNumber / Length), pseudoKnudsenNumber, skinFrictionDragCoefficient);
 
             _vesselIntakeRamDrag.ApplyIntakeRamDrag((float)machNumber, vessel.srf_velocity.normalized, (float)vessel.dynamicPressurekPa);
 
@@ -328,10 +328,10 @@ public void SimulateAeroProperties(out Vector3 aeroForce, out Vector3 aeroTorque
             float reynoldsPerLength = reynoldsNumber / (float)Length;
             float skinFriction = (float)FARAeroUtil.SkinFrictionDrag(reynoldsNumber, machNumber);
 
-            float pseudode LavalNumber = machNumber / (reynoldsNumber + machNumber);
+            float pseudoKnudsenNumber = machNumber / (reynoldsNumber + machNumber);
 
             for(int i = 0; i < _currentAeroSections.Count; i++)
-                _currentAeroSections[i].PredictionCalculateAeroForces(density, machNumber, reynoldsPerLength, pseudode LavalNumber, skinFriction, velocityWorldVector, center);
+                _currentAeroSections[i].PredictionCalculateAeroForces(density, machNumber, reynoldsPerLength, pseudoKnudsenNumber, skinFriction, velocityWorldVector, center);
 
             for (int i = 0; i < _legacyWingModels.Count; i++)
                 _legacyWingModels[i].PrecomputeCenterOfLift(velocityWorldVector, machNumber, density, center);

diff --git a/GameData/FerramAerospaceResearch/Plugins/FerramAerospaceResearch.dll b/GameData/FerramAerospaceResearch/Plugins/FerramAerospaceResearch.dll
diff --git a/GameData/FerramAerospaceResearch/Plugins/ferramGraph.dll b/GameData/FerramAerospaceResearch/Plugins/ferramGraph.dll