/**
* @author Lorenzo Attanasio
* @param mach
* @param ar
* @param semispan
* @param sweepHalfChordEq
* @param acToCgDistance
* @param wingMAC
* @param alpha0L
* @param cLalpha
* @param yStations
* @param clAlphaVsY
* @param chordsVsY
* @return
*/
public static double calcCM0LS(
double mach,
double ar,
double semispan,
double sweepHalfChordEq,
double acToCgDistance,
double wingMAC,
double alpha0L,
double cLalpha,
double[] yStations,
double[] clAlphaVsY,
double[] chordsVsY) {
return cLalpha
+ LiftCalc.calculateLiftCoefficientAtAlpha0(alpha0L, cLalpha) * (acToCgDistance / wingMAC);
}
