If the vertical plane of symmetry in the beam of P.21.3 is swept back by 25° as shown in plan in Fig. P.21.4, the span of 3 m is retained and the 40 kN load is applied as in P.21.3, calculate the flange and stringer loads and the shear flow distribution at a section 1.5 m from the built-in end.
As in S.21.3 and referring to Figs. P.21.4, S.21.4(a), and S.21.4(b),
Pz,1=−Pz,2=−133300NPz,3=Pz,5=−Pz,4=−Pz,6=−66650NThe solution now continues in Table S.21.4.
From Table S.21.4,
Then Sx,w=0,Sy,w=40−13.4=26.6kN
The qb shear flows are the same as in S.21.3, so taking moments about boom 2,
26.6×103×550=59.2×225×500+29.6×250×225+2×500×225qs,0from which qs,0=27.6 N/mm.
The final shear flows are then as shown in Fig.S.21.4(c).
Table S.21.4 | |||||||||||||||||||||
Boom | Pz,r(kN) | δxr/δz | δyr/δz | Px,r(kN) | Py,r(kN) | (kN)Pr | ξr(mm) | ηr(mm) | Px,rηr(kNm) | Py,rξr(kNm) | |||||||||||
1 | -133.3 | 0.47 | –0.025 | –62.7 | 3.3 | –147.3 | 250 | 112.5 | 7.05 | –0.83 | |||||||||||
2 | 133.3 | 0.47 | 0.025 | 62.7 | 3.3 | 147.3 | 250 | 112.5 | 7.05 | 0.83 | |||||||||||
3 | -66.7 | 0.47 | –0.025 | –31.3 | 1.7 | –73.7 | 0 | 112.5 | 3.52 | 0 | |||||||||||
4 | 66.7 | 0.47 | 0.025 | 31.3 | 1.7 | 73.7 | 0 | 112.5 | 3.52 | 0 | |||||||||||
5 | -66.7 | 0.47 | –0.025 | –31.3 | 1.7 | –73.7 | 250 | 112.5 | 3.52 | –0.42 | |||||||||||
6 | 66.7 | 0.47 | 0.025 | 31.3 | 1.7 | 73.7 | 250 | 112.5 | 3.52 | 0.42 |