/**
* @param wingAr
* @param verticalAr
* @param surfaceWing
* @param surfaceVertical
* @param sweepC2vertical
* @param clAlphaVertical
* @param mach
* @param kFv
* @param kWv
* @param kHv
* @return
*/
public static double calcCNbetaVerticalTail(
double wingAr,
double verticalAr,
double armVertical,
double wingSpan,
double surfaceWing,
double surfaceVertical,
double sweepC2vertical,
double clAlphaVertical,
double mach,
double kFv,
double kWv,
double kHv) {
return calcCNbetaVerticalTail(
LiftCalc.calculateCLalphaHelmboldDiederich(
verticalAr, clAlphaVertical, sweepC2vertical, mach),
kFv,
kWv,
kHv,
armVertical,
surfaceVertical,
surfaceWing,
wingSpan);
}
/**
* @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);
}
