/** * @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); }