Avoid divide by 0 in TubeCalc when velocity is 0 by setting CD to 0 in this case.
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@ -40,6 +40,11 @@ public abstract class TubeCalc extends RocketComponentCalc {
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public double calculatePressureCD(FlightConditions conditions,
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double stagnationCD, double baseCD, WarningSet warnings) {
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// If we aren't moving, treat CD as 0
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final double v = conditions.getVelocity();
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if (v < MathUtil.EPSILON)
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return 0;
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// Need to check for tube inner area 0 in case of rockets using launch lugs with
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// an inner radius of 0 to emulate rail guides (or just weird rockets, of course)
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double tubeCD = 0.0;
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@ -49,7 +54,6 @@ public abstract class TubeCalc extends RocketComponentCalc {
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final double p = conditions.getAtmosphericConditions().getPressure();
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final double t = conditions.getAtmosphericConditions().getTemperature();
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final double rho = conditions.getAtmosphericConditions().getDensity();
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final double v = conditions.getVelocity();
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// Reynolds number (note Reynolds number for the interior of a pipe is based on diameter,
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// not length (t))
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