4. For an aircraft in landing configuration at 0 m ISA (p=1.225kg/m) the following data indicated in the table below are known: W S [kN] [m] 10 16 [-] 0.100 5.5 Ae AB [-] Clmax [-] 1.6 CLg b [-] [-] 0.90 0.55 [7pt.] Calculate the total landing distance. VA/Vmin 1.3 (Use the energy method for the airborne phase where the average excess trust T-D is taken to be the average of the excess thrust at screen height and at touchdown.) VT/Vmin 1.2 YA [] 5.5 hs [m] 15