Civil Engineering Reference
In-Depth Information
Tank and loa-
bearing cross
section
Fig. 14.14
View of the contact section of the wing to the fuselage; only the central third is
designed as a load-bearing cross section and is simultaneously designed as a tank
Fig. 14.15
Nose landing gear; on the left in the extended position, on the
right
in the retracted
position; the hydraulic cylinder points forward in the direction of flight
