An aircraft weighing900kNwhen empty has a wing area of226 m2. It is to take off at velocity of550 km/hand angle of attack20â. Assume the airport is at4500 mabove sea level. The wing has the characteristics of an airfoil shown in the figure below(C1vsα). What is (i) the allowable weight of the cargo and (ii) induced drag coefficient if the wing span is30 m. The pressure variation in the atmosphere is given as: PRTCL=1,30kp=ps(1âTsBâz)BâRgsWhereRis the gas constant for air,Bis the lapse rate=dzdT=â km6.5 K,Ts=15âC,R=287J/K/kg, subscript s=sea-level. Ps=101.325kPa.gs=9.81 m/s/s