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This was some debug I put in while fixing the error in subsonic nose cone drag (#1063). It isn't needed any more, and dumps a wad of unnecessary output in our already voluminous debug logs.

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This commit is contained in:
JoePfeiffer 2022-03-07 14:43:39 -07:00
parent 1ff0ee9006
commit 533093f418
1 changed files with 0 additions and 13 deletions
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13
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
* the subsonic region, if the values are non-zero.
@ -404,9 +394,6 @@ public class SymmetricComponentCalc extends RocketComponentCalc {
double cdMach0 = 0.8 * pow2(sinphi);
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
if ((cdMach0 >= minValue - 0.01) || (minDeriv <= 0.01)) {
return;