Modify FinSetCalc to only produce result for one fin, to be summed in

BarrowmanCalculator

Modify BarrowmanCalculator to actually sum fin nonaxial forces

Modify FinSetCalcTest to sum fins in test3Fin() and test4Fin()

Extra bonus:  if at some point we allow fins to be other than radially
symmetrical, this code should still work (not tested)

core/src/net/sf/openrocket/aerodynamics/AerodynamicForces.java

@@ -392,7 +392,6 @@ public class AerodynamicForces implements Cloneable, Monitorable {
 	}
 
 	public AerodynamicForces merge(AerodynamicForces other) {
-
 		this.cp = cp.average(other.getCP());
 		this.CNa = CNa + other.getCNa();
 		this.CN = CN + other.getCN();

core/src/net/sf/openrocket/aerodynamics/BarrowmanCalculator.java

@@ -194,12 +194,6 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 				final ArrayList<InstanceContext> contextList = entry.getValue();
 
 				for(InstanceContext context: contextList ) {
-					// since FinSetCalc calculates forces for entire FinSet
-					// only consider first fin in each set (happily,
-					// in each instance of a PodSet or similar
-					// instanceable RocketComponent with childre, the
-					// child FinSets all start numbering with 0
-					if (!(comp instanceof FinSet) || (context.instanceNumber == 0)) {
 					AerodynamicForces instanceForces = new AerodynamicForces().zero();
 					
 					calcObj.calculateNonaxialForces(conditions, context.transform, instanceForces, warnings);
@@ -217,7 +211,6 @@ public class BarrowmanCalculator extends AbstractAerodynamicCalculator {
 				}
 			}
 		}
-		}
 
 		// System.err.println("assemblyForces=" + assemblyForces);
 		return assemblyForces;

core/src/net/sf/openrocket/aerodynamics/barrowman/FinSetCalc.java

@@ -117,18 +117,7 @@ public class FinSetCalc extends RocketComponentCalc {
 		double angle = baseRotation + transform.getXrotation();
 		
 		// Compute basic CNa without interference effects
-		if (finCount == 1 || finCount == 2) {
+		cna = cna1 * MathUtil.pow2(Math.sin(theta - angle));
-			// Basic CNa from geometry
-			double mul = 0;
-			for (int i = 0; i < finCount; i++) {
-				mul += MathUtil.pow2(Math.sin(theta - angle));
-				angle += 2 * Math.PI / finCount;
-			}
-			cna = cna1 * mul;
-		} else {
-			// Basic CNa assuming full efficiency
-			cna = cna1 * finCount / 2.0;
-		}
 		
 		//		logger.debug("Component cna = {}", cna);
 		

core/test/net/sf/openrocket/aerodynamics/FinSetCalcTest.java

@@ -38,6 +38,27 @@ public class FinSetCalcTest {
 //		}
 	}
 
+	private AerodynamicForces sumFins(TrapezoidFinSet fins, Rocket rocket)
+	{
+		FlightConfiguration config = rocket.getSelectedConfiguration();
+		FlightConditions conditions = new FlightConditions(config);
+		WarningSet warnings = new WarningSet();
+		AerodynamicForces assemblyForces = new AerodynamicForces().zero();
+		AerodynamicForces componentForces = new AerodynamicForces();
+
+		FinSetCalc calcObj = new FinSetCalc( fins );
+		
+		// Need to sum forces for fins
+		for (Integer i = 0; i < fins.getFinCount(); i++) {
+			calcObj.calculateNonaxialForces(conditions,
+											Transformation.rotate_x(Math.PI * i / fins.getFinCount()),
+											componentForces, warnings);
+			assemblyForces.merge(componentForces);
+		}
+
+		return assemblyForces;
+	}
+		
 	@Test
 	public void test3Fin() {
 		Rocket rocket = TestRockets.makeEstesAlphaIII();
@@ -50,17 +71,8 @@ public class FinSetCalcTest {
 		assertEquals(" Estes Alpha III fins have wrong sweep: ", 0.02, fins.getSweep(), EPSILON);
 		assertEquals(" Estes Alpha III fins have wrong height: ", 0.05, fins.getHeight(), EPSILON);
 
-		FlightConfiguration config = rocket.getSelectedConfiguration();
+		// get the forces for the three fins
-		Transformation transform = Transformation.IDENTITY;
+		AerodynamicForces forces = sumFins(fins, rocket);
-		FlightConditions conditions = new FlightConditions(config);
-		WarningSet warnings = new WarningSet();
-		AerodynamicForces forces = new AerodynamicForces();
-		FinSetCalc calcObj = new FinSetCalc( fins );
-		
-		
-		// vvv TEST MEH! vvv 
-		calcObj.calculateNonaxialForces(conditions, transform, forces, warnings);
-		// ^^^ 
 
 		double exp_cna_fins = 24.146933;
 		double exp_cpx_fins = 0.0193484;
@@ -85,17 +97,8 @@ public class FinSetCalcTest {
 		assertEquals(" Estes Alpha III fins have wrong sweep: ", 0.02, fins.getSweep(), EPSILON);
 		assertEquals(" Estes Alpha III fins have wrong height: ", 0.05, fins.getHeight(), EPSILON);
 
-		FlightConfiguration config = rocket.getSelectedConfiguration();
+		// get the forces for the four fins
-		Transformation transform = Transformation.IDENTITY;
+		AerodynamicForces forces = sumFins(fins, rocket);
-		FlightConditions conditions = new FlightConditions(config);
-		WarningSet warnings = new WarningSet();
-		AerodynamicForces forces = new AerodynamicForces();
-		FinSetCalc calcObj = new FinSetCalc( fins );
-		
-		
-		// vvv TEST MEH! vvv 
-		calcObj.calculateNonaxialForces(conditions, transform, forces, warnings);
-		// ^^^ 
 		
 		double exp_cna_fins = 32.195911;
 		double exp_cpx_fins = 0.0193484;