R16-6. If the cantilever beam has a constant thickness t, determine the deflection at cnd A. The beam is made of material having a modulus of clasticity E.

6-122 Segment A of the composdte heam is made from 2014-T6 aluminum alloy and segment Bs A-36 steel. If w - 0.9 kip/, determine the absolute maximum bending stress developed in the aluminum and steed. Skelch the stress distribution on the cross section. 6-123. SegmentA of the composite beam is made trom 2014-T6 aluminum alkoy and segment B s A-36 steel. The alowable bending stress for the aluminum and steel are (a)¬15 ksi and (a -22 k.Determine the maximum alowahle Intensity w of the uniform distributed kad. -15 h Probs. 6-122/123

Determine the deflection of end A if E = 200 GPa and I = 65 x 10^6 mm^4

Determine the deflection at x=2.5 m and x=8.