An Airbus A 320 lands on its main landing gear with a deceleration of 1.5g. Which statement is correct for the above mentioned landing A) The spar webs are loaded in tension. B) All spar caps are loaded in shear. C) All spar caps are loaded in tension. D)The spar webs are loaded in shear
Which of the following statements on sheet material and shell structures are TRUE?
A) A sandwich structure is an example of a monocoque structure.
B) A hat-stiffener provides less support against compression than a z-stiffener.
C) Corrosion does not occur in sandwich structures.
D) A sheet provides the diagonal function when loaded in shear.
An Airbus A 320 lands on its main landing gear with a deceleration of 1.5g.
Which statement is correct for the above mentioned landing
A) The spar webs are loaded in tension.
B) All spar caps are loaded in shear.
C) All spar caps are loaded in tension.
D)The spar webs are loaded in shear
Consider a Boeing 787 and assume the fuselage cross-section to be circular with a diameter d=5.9m, a skin thickness t=2mm, and isotropic material properties of E=60GPa and ν=0.28.
The vertical tail plane applies a torsional moment of the rear fuselage, inducing a shear flow in the rear fuselage skin.
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