Jet transporthas the takaff weigh w8s.00 b. given the landing field length ) find the mathematic expression for the thrust to-weight ratio as the function of the )a jet transport has t at h-2500 n altitude on a 96 f hot day losading and the maximum lifh coefficient at take-offcbaeon minimum required thrast-to-weight ratio based on the take-off distance (e) detennine the take-off wing lowding and the masimum lift coefficient at landing, take-off wing the take-off distance sizing requirements sizing requirements