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Truss ILDs for L0U1, L0L1, U2L2

Short answer

L0U1 ILD: always compression, ordinate = −1.414 R_L0, max −1.179 at L1. L0L1 always tension, ordinate = +R_L0, max +0.833 at L1. U2L2: force = −shear in panel L2L3; bottom-chord loading gives +0.333 at L2, −0.500 at L3; top-chord gives −0.667 at U2.

Draw influence line diagram for members L0U1L_0U_1, L0L1L_0L_1 and U2L2U_2L_2 when unit load moves on the chords. [Figure: truss with bottom joints L0L_0 to L6L_6 and top joints U1U_1 to U5U_5, 6 panels of 5 m = 30 m, height 5 m, L0L_0 hinge, L6L_6 roller.]

Assumed truss (figure not available): Pratt truss, 6 panels of 5 m (span 30 m), height 5 m; verticals UiLiU_iL_i and diagonals U1L2U_1L_2, U2L3U_2L_3, U4L3U_4L_3, U5L4U_5L_4; end posts L0U1L_0U_1 and L6U5L_6U_5 at 45°. L0L_0 hinge, L6L_6 roller. Reaction for unit load at xx from L0L_0: RL0=(30−x)/30R_{L_0} = (30-x)/30.

Method

  • L0U1L_0U_1 (end post): joint L0L_0, vertical equilibrium: Fsin⁡45∘=−RL0F\sin45^\circ = -R_{L_0}, so FL0U1=−1.414 RL0F_{L_0U_1} = -1.414\,R_{L_0} (always compression).
  • L0L1L_0L_1: horizontal equilibrium at L0L_0: FL0L1=−FL0U1cos⁡45∘=+RL0F_{L_0L_1} = -F_{L_0U_1}\cos45^\circ = +R_{L_0} (always tension).
  • U2L2U_2L_2 (vertical): the section through U2U3U_2U_3, U2L3U_2L_3 and L2L3L_2L_3 gives the diagonal FU2L3=2 VF_{U_2L_3} = \sqrt2\,V, where VV is the shear in panel L2L3L_2L_3 (left forces upward positive). At the unloaded joint U2U_2 the vertical balances the diagonal: FU2L2=−FU2L3/2=−VF_{U_2L_2} = -F_{U_2L_3}/\sqrt2 = -V. For a unit load at L2L_2: V=23−1=−13V = \tfrac23 - 1 = -\tfrac13, so FU2L2=+0.333F_{U_2L_2} = +0.333. For a unit load on the top chord at U2U_2, the load itself is added at the joint, which gives −0.667-0.667.

Ordinates when the unit load moves on the bottom chord (+ tension)

MemberL0L1L2L3L4L5L6
L0U10.000-1.179-0.943-0.707-0.471-0.2360.000
L0L10.0000.8330.6670.5000.3330.1670.000
U2L20.0000.1670.333-0.500-0.333-0.1670.000

Ordinates when the unit load moves on the top chord

MemberU1U2U3U4U5
L0U1-1.179-0.943-0.707-0.471-0.236
L0L10.8330.6670.5000.3330.167
U2L20.167-0.667-0.500-0.333-0.167

Shapes (bottom-chord loading)

  • L0U1L_0U_1: always compression. 0 at L0L_0 (load directly on the support), peak −1.179-1.179 at L1L_1, then a straight line decreasing to 0 at L6L_6. Beyond L1L_1 the ordinate is −1.414 RL0-1.414\,R_{L_0}.
  • L0L1L_0L_1: always tension. 0 at L0L_0, peak +0.833+0.833 at L1L_1, then falling linearly to 0 at L6L_6 (ordinate =RL0=R_{L_0}).
  • U2L2U_2L_2: +0.167+0.167 at L1L_1, +0.333+0.333 at L2L_2, −0.5-0.5 at L3L_3, then −0.333-0.333, −0.167-0.167 and 0. The sign changes between L2L_2 and L3L_3, at x=10+5×0.3330.833=12x = 10 + 5\times\frac{0.333}{0.833} = 12 m from L0L_0, so the vertical is stressed in both tension and compression (the part of the ILD with a negative area is larger).
  • With top-chord loading, the ordinates of L0U1L_0U_1 and L0L1L_0L_1 are the same linear functions of RL0R_{L_0} (taken at the top joints), while U2L2U_2L_2 takes −0.667-0.667 at U2U_2, since the load acts directly on the vertical.

✓ Answer checked by Claude Opus 5.5 (high effort)

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