From: plaa <plaa@180e2498-e6e9-4542-8430-84ac67f01cd8>
Date: Sun, 4 Sep 2011 17:54:10 +0000 (+0000)
Subject: renamed private method
X-Git-Tag: upstream/1.1.9^2~15
X-Git-Url: https://git.gag.com/?a=commitdiff_plain;h=90d06d455ef16eb3ea48c5c7a5fba4bc1e30e61f;p=debian%2Fopenrocket

renamed private method

git-svn-id: https://openrocket.svn.sourceforge.net/svnroot/openrocket/trunk@169 180e2498-e6e9-4542-8430-84ac67f01cd8
---

diff --git a/src/net/sf/openrocket/aerodynamics/BarrowmanCalculator.java b/src/net/sf/openrocket/aerodynamics/BarrowmanCalculator.java
index dac1c83d..be139e14 100644
--- a/src/net/sf/openrocket/aerodynamics/BarrowmanCalculator.java
+++ b/src/net/sf/openrocket/aerodynamics/BarrowmanCalculator.java
@@ -58,7 +58,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	public Coordinate getCP(Configuration configuration, FlightConditions conditions,
 			WarningSet warnings) {
 		checkCache(configuration);
-		AerodynamicForces forces = getNonAxial(configuration, conditions, null, warnings);
+		AerodynamicForces forces = calculateNonAxialForces(configuration, conditions, null, warnings);
 		return forces.getCP();
 	}
 	
@@ -83,7 +83,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 		
 
 		// Calculate non-axial force data
-		AerodynamicForces total = getNonAxial(configuration, conditions, map, warnings);
+		AerodynamicForces total = calculateNonAxialForces(configuration, conditions, map, warnings);
 		
 
 		// Calculate friction data
@@ -124,7 +124,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 			warnings = ignoreWarningSet;
 		
 		// Calculate non-axial force data
-		AerodynamicForces total = getNonAxial(configuration, conditions, null, warnings);
+		AerodynamicForces total = calculateNonAxialForces(configuration, conditions, null, warnings);
 		
 		// Calculate friction data
 		total.setFrictionCD(calculateFrictionDrag(configuration, conditions, null, warnings));
@@ -150,7 +150,7 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 	/*
 	 * Perform the actual CP calculation.
 	 */
-	private AerodynamicForces getNonAxial(Configuration configuration, FlightConditions conditions,
+	private AerodynamicForces calculateNonAxialForces(Configuration configuration, FlightConditions conditions,
 			Map<RocketComponent, AerodynamicForces> map, WarningSet warnings) {
 		
 		checkCache(configuration);