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Truss: force method, double-diagonal truss

Short answer

Force method with redundants AC and CF forces. Flexibility coefficients computed from virtual work, compatibility equations solved. Final forces: AE=+26.05 kN, EF=+17.78 kN, BC=-2.70 kN, CD=+9.03 kN, AB=-3.61 kN, CE=-18.23 kN, DF=-14.62 kN, BE=+4.51 kN, AC=-10.08 kN, CF=-29.64 kN, ED=+18.28 kN (positive tension).

Determine the forces in all members of the truss shown in figure below using the force method. AE is constant for all members. [Figure: truss with joints A, B (left), C, D (top) and E, F (bottom); panels 3 m + 3 m wide and 4 m high, double diagonals; 50 kN downward at C and 20 kN horizontal at D; A hinged, F roller.]

Reading of the figure: bottom joints A (0, 0), E (3, 0), F (6, 0); top joints B (0, 4), C (3, 4), D (6, 4). Members: chords AE, EF, BC, CD; verticals AB, CE, DF; and two crossing diagonals in each panel (BE, AC and CF, ED). A is hinged, F is a roller. Loads: 50 kN downward at C and 20 kN horizontal at D (towards the right). AEAE is constant.

m=11m = 11, j=6j = 6, r=3r = 3, so Ds=11+3−12=2D_s = 11 + 3 - 12 = 2. Take X1X_1 = force in AC and X2X_2 = force in CF (tension +).

Reactions

ΣMA=0\Sigma M_A = 0: VF(6)=50(3)+20(4)⇒VF=38.333V_F(6) = 50(3) + 20(4) \Rightarrow V_F = 38.333 kN (↑\uparrow); VA=50−38.333=11.667V_A = 50 - 38.333 = 11.667 kN (↑\uparrow); HA=20H_A = 20 kN (←\leftarrow).

Force tables (tension +)

MemberLL (m)S0S_0n1n_1n2n_2Final SS
AE3.000+20.000-0.6000.000+26.046
EF3.0000.0000.000-0.600+17.785
BC3.000-8.750-0.6000.000-2.704
CD3.000-8.7500.000-0.600+9.035
AB4.000-11.667-0.8000.000-3.606
CE4.000-50.000-0.800-0.800-18.226
DF4.000-38.3330.000-0.800-14.620
BE5.000+14.583+1.0000.000+4.507
AC5.0000.000+1.0000.000-10.076
CF5.0000.0000.000+1.000-29.641
ED5.000+47.9170.000+1.000+18.275

Flexibility coefficients (in 1/AE1/AE units)

f11=∑n12L=17.280,f22=∑n22L=17.280,f12=∑n1n2L=2.560Δ10=∑S0n1L=250.000,Δ20=∑S0n2L=538.000\begin{aligned} f_{11} &= \sum n_1^2L = 17.280, \quad f_{22} = \sum n_2^2L = 17.280, \quad f_{12} = \sum n_1n_2L = 2.560 \\ \Delta_{10} &= \sum S_0n_1L = 250.000, \quad \Delta_{20} = \sum S_0n_2L = 538.000 \end{aligned}

Compatibility

17.280 X1+2.560 X2=−(250.000)2.560 X1+17.280 X2=−(538.000)\begin{aligned} 17.280\,X_1 + 2.560\,X_2 &= -(250.000) \\ 2.560\,X_1 + 17.280\,X_2 &= -(538.000) \end{aligned} X1=SAC=−10.08 kN,X2=SCF=−29.64 kNX_1 = S_{AC} = -10.08\ \text{kN},\qquad X_2 = S_{CF} = -29.64\ \text{kN}

Final member forces S=S0+n1X1+n2X2S = S_0 + n_1X_1 + n_2X_2

MemberForce (kN)Nature
AE+26.05tension
EF+17.78tension
BC-2.70compression
CD+9.03tension
AB-3.61compression
CE-18.23compression
DF-14.62compression
BE+4.51tension
AC-10.08compression
CF-29.64compression
ED+18.28tension

Answer: AE =+26.05= +26.05, EF =+17.78= +17.78, BC =−2.70= -2.70, CD =+9.03= +9.03, AB =−3.61= -3.61, CE =−18.23= -18.23, DF =−14.62= -14.62, BE =+4.51= +4.51, AC =−10.08= -10.08, CF =−29.64= -29.64, ED =+18.28= +18.28 kN (positive = tension).

✓ Answer checked by Claude Opus 5.5 (high effort)

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