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Truss ILDs for LC, LK, LD, lower chord

Short answer

Influence ordinates: LK is entirely compression, peak −1.125 at D; LD changes sign, maximum tension 0.625 at D, maximum compression −0.417 at C; LC tension peak 0.333 at C, compression peak −0.5 at D, sign change at 14.4 m from A.

Draw influence line diagram for the members LC, LK and LD when the load moves in the lower chord of the given truss as shown in figure. [Figure: truss with bottom joints A, B, C, D, E, F, G (6 panels of 6 m = 36 m), top joints N, M, L, K, J, I, H, height 8 m; A hinge, G roller.]

Assumed truss (Pratt type): bottom joints AA–GG, top joints N,M,L,K,J,I,HN, M, L, K, J, I, H directly above them, 6 panels of 6 m (span 36 m), height 8 m; verticals at every joint; diagonals NBNB, MCMC, LDLD, JDJD, IEIE, HFHF (sloping down towards the centre). AA hinge, GG roller. The load moves on the lower chord. Reactions: RA=36−x36R_A = \dfrac{36-x}{36}, RG=x36R_G = \dfrac{x}{36}. The diagonal LDLD has length 1010 m, sin⁡θ=0.8\sin\theta = 0.8.

Member LK (top chord, panel CDCD)

Section through LKLK, LDLD and CDCD (panel CDCD); LDLD and CDCD meet at DD (x=18x = 18 m), so take moments about DD (lever arm 8 m): FLK=−MD8F_{LK} = -\dfrac{M_D}{8}.

  • Load right of DD: FLK=−18RA8=−2.25RAF_{LK} = -\dfrac{18R_A}{8} = -2.25R_A; load left of CC: FLK=−18RG8=−2.25RGF_{LK} = -\dfrac{18R_G}{8} = -2.25R_G (compression).

Member LD (diagonal)

Same section: the panel shear is carried by the diagonal, FLD=±V0.8F_{LD} = \pm\dfrac{V}{0.8}.

  • Load right of DD: FLD=+RA0.8=1.25RAF_{LD} = +\dfrac{R_A}{0.8} = 1.25R_A (tension).
  • Load left of CC: FLD=−1.25RGF_{LD} = -1.25R_G (compression).

Member LC (vertical)

At the unloaded top joint LL the vertical balances the vertical component of the diagonal: FLC=−0.8 FLDF_{LC} = -0.8\,F_{LD}.

Ordinates (per unit load; + tension, − compression)

MemberABCDEFG
LC0.0000.1670.333-0.500-0.333-0.1670.000
LK0.000-0.375-0.750-1.125-0.750-0.3750.000
LD0.000-0.208-0.4170.6250.4170.2080.000

Shapes

  • LK: compression only, triangle with peak −1.125-1.125 under DD (centre).
  • LD: compression (peak −0.417-0.417 at CC) for load left of the panel, tension (peak +0.625+0.625 at DD) for load to the right; the neutral point is at x=12+6×0.4170.417+0.625=14.4x = 12+6\times\frac{0.417}{0.417+0.625} = 14.4 m from AA.
  • LC: tension for load on the left (peak +0.333+0.333 at CC), compression to the right (peak −0.5-0.5 at DD); the sign change lies between CC and DD at x=12+6×0.3330.333+0.5=14.4x = 12 + 6\times\frac{0.333}{0.333+0.5} = 14.4 m.

✓ Answer checked by Claude Opus 5.5 (high effort)

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