Merge branch 'openrocket:unstable' into generalize-automatic-tube-fin-radius
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commit
f0d7566690
@ -660,7 +660,7 @@ public class FinSetCalc extends RocketComponentCalc {
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// Airfoil assumed to have zero base drag
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// Scale to correct reference area
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cd *= cd * span * thickness / conditions.getRefArea();
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cd *= span * thickness / conditions.getRefArea();
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return cd;
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}
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