Whoops, don't use compressibility correction at supersonic flow
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@ -468,7 +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() * conditions.getBeta();
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double vel = conditions.getVelocity();
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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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