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Merge pull request #1232 from JoePfeiffer/cleanup-SymmetricComponentCalc-debug

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Remove unnecessary debug from SymmetricComponentCalc
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Joe Pfeiffer 2022-03-07 15:30:34 -07:00 committed by GitHub
commit 46017a0e8b
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1 changed files with 0 additions and 13 deletions
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core/src/net/sf/openrocket/aerodynamics/barrowman/SymmetricComponentCalc.java
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@ -379,16 +379,6 @@ public class SymmetricComponentCalc extends RocketComponentCalc {
} }
} }
// dump transonic/supersonic knots, in a format easily imported into python
String vel = "vel = [ ";
String cd = "cd = [ ";
for (double m : interpolator.getXPoints()) {
vel = vel + m + ", ";
cd = cd + interpolator.getValue(m) + ", ";
}
log.debug(vel + "]");
log.debug(cd + "]");
/* /*
* Now the transonic/supersonic region is ok. We still need to interpolate * Now the transonic/supersonic region is ok. We still need to interpolate
* the subsonic region, if the values are non-zero. * the subsonic region, if the values are non-zero.
@ -403,9 +393,6 @@ public class SymmetricComponentCalc extends RocketComponentCalc {
double cdMach0 = 0.8 * pow2(sinphi); double cdMach0 = 0.8 * pow2(sinphi);
double minDeriv = (interpolator.getValue(min + 0.01) - minValue) / 0.01; double minDeriv = (interpolator.getValue(min + 0.01) - minValue) / 0.01;
log.debug("cdMach0 = " + cdMach0);
log.debug("minDeriv = " + minDeriv);
// These should not occur, but might cause havoc for the interpolation // These should not occur, but might cause havoc for the interpolation
if ((cdMach0 >= minValue - 0.01) || (minDeriv <= 0.01)) { if ((cdMach0 >= minValue - 0.01) || (minDeriv <= 0.01)) {