For both the EF 2000 and J-7 aircrafts main landing gears are attached to wings.
However, J-7 's wing has spar frame structure, whereas EF 2000's wing has Multiweb structure.
With regards to landing gear arrangement, what are the differences between wing and fuselage structural design of both fighters. Moreover, how the landing gear loads are transmitted to fuselage for both aircrafts.
However, J-7 's wing has spar frame structure, whereas EF 2000's wing has Multiweb structure.
With regards to landing gear arrangement, what are the differences between wing and fuselage structural design of both fighters. Moreover, how the landing gear loads are transmitted to fuselage for both aircrafts.
