import net.sf.openrocket.aerodynamics.barrowman.RocketComponentCalc;
import net.sf.openrocket.rocketcomponent.Configuration;
import net.sf.openrocket.rocketcomponent.ExternalComponent;
+import net.sf.openrocket.rocketcomponent.ExternalComponent.Finish;
import net.sf.openrocket.rocketcomponent.FinSet;
import net.sf.openrocket.rocketcomponent.RocketComponent;
import net.sf.openrocket.rocketcomponent.SymmetricComponent;
-import net.sf.openrocket.rocketcomponent.ExternalComponent.Finish;
import net.sf.openrocket.util.Coordinate;
import net.sf.openrocket.util.MathUtil;
import net.sf.openrocket.util.PolyInterpolator;
// System.out.printf("constant Cf=%f ",Cf);
} else if (Re < 5.39e5) {
// Fully laminar
- Cf = 1.328 / Math.sqrt(Re);
+ Cf = 1.328 / MathUtil.safeSqrt(Re);
// System.out.printf("basic Cf=%f ",Cf);
} else {
// Transitional