FuselageAnalysis.mlx

https://docs.google.com/spreadsheets/d/1d45Qfu4blAfdZ_Woj6W3JtkMQmG359kJ1iGoYMM78Vc/edit?gid=0#gid=0

mfw = mfwASA + x(4(mfwCFtow )+ (mfwFG + mfwAE))

Code assumes correction factor x = 1

Find value of x