please show all work! i'll rate! answers are given Datum |--150" - 5" -400" 80"- 90"...

Question

Question

please show all work! i'll rate!

answers are given

Datum |--150 - 5 -400 80- 90 280 [2] Imagine the wings center of lift is at the aircraft cg, and estimate the ultimate

VMGW U_d 17.10 kips , WMGW =4.50 kip _U_U =11.66 lb/int, 2. W fus_twd =82.9 lb/in !, W fus_aft 3 =622 Line 1 M -222 in Line

engineering Mechanical-Engineering

Answer 1

Answer #1

Please clear me the data of pt 1 and pt 3.

It will not so clear and also unit is not clear.

Pls update it clearly.

Answer 2