Also apply Prandtl correction at supersonic speed
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				@ -468,8 +468,7 @@ public class FinSetCalc extends RocketComponentCalc {
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							conditions.getVelocity() * conditions.getBeta());
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		}
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		if (mach >= CNA_SUPERSONIC) {
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			double vel = conditions.getVelocity();
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			double vel = conditions.getVelocity() * conditions.getBeta();
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			double k1 = K1.getValue(mach);
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			double k2 = K2.getValue(mach);
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			double k3 = K3.getValue(mach);
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