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Truss ILDs for AB, CD, EJ, FH

Short answer

Using section methods, the influence ordinates per unit load on the bottom chord are: AB: 0, −0.6, −0.45, −0.3, −0.15, 0, 0.15; CD: 0, −0.3, −0.6, −0.9, −0.45, 0, 0.45; EJ: 0, 0.2, 0.4, 0.6, 0.8, 0, 0.2; FH: 0, 0, 0, 0, 0, 0, 1.25. Member forces are computed as sum of actual loads multiplied by corresponding ordinates or UDL areas.

Using influence line diagram, obtain member force in AB, CD, EJ and FH for the following loaded pin-jointed truss as shown in figure below. [Figure: pin-jointed truss with top joints A to G and bottom joints N, M, L, K, J, I, H, 6 panels of 3 m = 18 m, height 4 m; N hinge, I roller; verticals and diagonals as drawn.]

Assumed truss (figure not available): top joints A,B,C,D,E,F,GA, B, C, D, E, F, G (left to right) directly above bottom joints N,M,L,K,J,I,HN, M, L, K, J, I, H, 6 panels of 3 m (18 m overall), height 4 m. Verticals at all joints; diagonals AMAM, BLBL, CKCK, DJDJ, EIEI, FHFH (all sloping down to the right). Supports as given: NN hinge and II roller (x=15x = 15 m), so the last panel IHIH (members FGFG, GHGH, FHFH, IHIH) overhangs 3 m beyond the roller. The loads are not given in the text, so the ILDs are drawn for a unit load on the bottom chord at xx from NN:

RN=15−x15,RI=x15(0≤x≤18)R_N = \frac{15-x}{15}, \qquad R_I = \frac{x}{15} \qquad (0\le x\le 18)

For a load at HH: RN=−0.2R_N = -0.2, RI=1.2R_I = 1.2. Diagonal length 32+42=5\sqrt{3^2+4^2} = 5 m, sin⁡θ=0.8\sin\theta = 0.8.

Method

  • AB (top chord, panel NMNM): section through ABAB, AMAM, NMNM; moments about MM (x=3x=3, where AMAM and NMNM meet), lever arm 4 m: for a load at or right of MM, FAB=−3RN4=−0.75RNF_{AB} = -\dfrac{3R_N}{4} = -0.75R_N; for a load at NN, 0.
  • CD (top chord, panel LKLK): section through CDCD, CKCK, LKLK; moments about KK (x=9x=9): load at or right of KK: FCD=−9RN4F_{CD} = -\dfrac{9R_N}{4}; load at or left of LL (right part, only RIR_I at 6 m from KK): FCD=−6RI4=−1.5RIF_{CD} = -\dfrac{6R_I}{4} = -1.5R_I.
  • EJ (vertical): at the unloaded top joint EE, FEJ=−0.8FEIF_{EJ} = -0.8F_{EI}, and FEI=V/0.8F_{EI} = V/0.8 from the shear VV in panel JIJI, so FEJ=−VF_{EJ} = -V. For a load at or left of JJ: V=RN−1V = R_N - 1, so FEJ=1−RN=x15F_{EJ} = 1 - R_N = \dfrac{x}{15}; for a load at or right of II: FEJ=−RNF_{EJ} = -R_N (0 at II, +0.2+0.2 at HH).
  • FH (diagonal, overhang panel IHIH): joint GG is unloaded and has only the two non-collinear members FGFG and GHGH, so FFG=FGH=0F_{FG} = F_{GH} = 0. At joint HH the remaining members are IHIH and FHFH. For a load left of II, HH is unloaded and FFH=0F_{FH} = 0. For the load at HH: 0.8 FFH=10.8\,F_{FH} = 1, so FFH=+1.25F_{FH} = +1.25 (tension).

Ordinates (per unit load on the bottom chord; + tension, − compression)

MemberNMLKJIH
AB0.000-0.600-0.450-0.300-0.1500.000+0.150
CD0.000-0.300-0.600-0.900-0.4500.000+0.450
EJ0.0000.2000.4000.6000.8000.0000.200
FH0.0000.0000.0000.0000.0000.0001.250

Shapes

  • AB: 0 at NN, compression peak −0.6-0.6 at MM, decreasing linearly to 0 at the roller II, then tension on the overhang (+0.15+0.15 at HH).
  • CD: compression, a triangle with peak −0.9-0.9 under KK, zero at II, then tension on the overhang (+0.45+0.45 at HH).
  • EJ: tension, rising linearly to +0.8+0.8 at JJ, falling to 0 at II, then rising again to +0.2+0.2 at HH.
  • FH: zero from NN to II, then rising linearly to +1.25+1.25 (tension) at HH.

The force in any member for the actual loads is F=∑P yF = \sum P\,y (concentrated loads) or w×w\times area (UDL), using these ordinates.

✓ Answer checked by Claude Opus 5.5 (high effort)

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