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Slope deflection: beam with rotations and settlements

Short answer

Using slope-deflection with given support rotations and settlements, joint rotations are θ_b = 0.001993 rad, θ_c = -0.001993 rad. Final end moments: M_ab = -62.61, M_ba = -27.72, M_bc = 27.72, M_cb = -27.72, M_cd = 27.72, M_dc = 62.61 kN·m.

Use the slope-direction (slope deflection) method to analyze the continuous beam shown in the figure. Draw free body diagram, BMD and SFD. The support "a" rotates by 0.001 radian clockwise and support "b" rotates by 0.001 radian anticlockwise. Support "b" and "c" both settle down by 10 mm. [Figure: beam a-b-c-d, a and d fixed; 20 kN at 2 m from a (ab = 2 m + 2 m, 3EI); bc = 5 m (4EI) with 2 kN/m UDL; cd = 2 m + 2 m (3EI) with 20 kN at mid-span.]

Assumptions

  • EIEI is not given. Take EI=10,000EI = 10{,}000 kN·m² (the moments caused by the support rotation and settlement scale with EIEI; load moments do not).
  • "Support b rotates" is read as a typing slip for the other fixed support d (b is a free interior joint), so the prescribed rotations are θa=0.001\theta_a = 0.001 rad clockwise and θd=0.001\theta_d = 0.001 rad anticlockwise. The joints bb and cc rotate freely and settle 10 mm.
  • Spans: ab = 4 m (3EI3EI), bc = 5 m (4EI4EI), cd = 4 m (3EI3EI). Clockwise end moments are positive.

Data

  • Chord rotations (clockwise +): ψab=0.01/4=+0.0025\psi_{ab} = 0.01/4 = +0.0025, ψbc=0\psi_{bc} = 0, ψcd=−0.01/4=−0.0025\psi_{cd} = -0.01/4 = -0.0025.
  • FEM: ab: ±PL/8=±10\pm PL/8 = \pm 10; bc: ±wL2/12=±2×25/12=±4.1667\pm wL^2/12 = \pm 2\times 25/12 = \pm 4.1667; cd: ±10\pm 10.
  • θa=+0.001\theta_a = +0.001, θd=−0.001\theta_d = -0.001; unknowns θb\theta_b, θc\theta_c.

Slope-deflection equations

Mnear=FEM+2EIL(2θnear+θfar−3ψ)M_{near} = FEM + \dfrac{2EI}{L}(2\theta_{near} + \theta_{far} - 3\psi)

Mab=−10+15000(2×0.001+θb−0.0075)=−92.5+15000 θbMba=+10+15000(2θb+0.001−0.0075)=−87.5+30000 θbMbc=−4.1667+16000(2θb+θc)Mcb=+4.1667+16000(2θc+θb)Mcd=−10+15000(2θc−0.001+0.0075)=87.5+30000 θcMdc=+10+15000(−0.002+θc+0.0075)=92.5+15000 θc\begin{aligned} M_{ab} &= -10 + 15000(2\times0.001 + \theta_b - 0.0075) = -92.5 + 15000\,\theta_b \\ M_{ba} &= +10 + 15000(2\theta_b + 0.001 - 0.0075) = -87.5 + 30000\,\theta_b \\ M_{bc} &= -4.1667 + 16000(2\theta_b + \theta_c) \\ M_{cb} &= +4.1667 + 16000(2\theta_c + \theta_b) \\ M_{cd} &= -10 + 15000(2\theta_c - 0.001 + 0.0075) = 87.5 + 30000\,\theta_c \\ M_{dc} &= +10 + 15000(-0.002 + \theta_c + 0.0075) = 92.5 + 15000\,\theta_c \end{aligned}

Joint equilibrium

Mba+Mbc=0:  62000 θb+16000 θc=91.667Mcb+Mcd=0:  16000 θb+62000 θc=−91.667\begin{aligned} M_{ba} + M_{bc} = 0 &: \; 62000\,\theta_b + 16000\,\theta_c = 91.667 \\ M_{cb} + M_{cd} = 0 &: \; 16000\,\theta_b + 62000\,\theta_c = -91.667 \end{aligned}

Solving: θb=+0.0019928\theta_b = +0.0019928 rad (clockwise), θc=−0.0019928\theta_c = -0.0019928 rad.

Final end moments (kN·m)

EndMomentMeaning
MabM_{ab}-62.61hogging (tension top) at a
MbaM_{ba}-27.72sagging (tension bottom) at b
MbcM_{bc}+27.72sagging at b
McbM_{cb}-27.72sagging at c
McdM_{cd}+27.72sagging at c
MdcM_{dc}+62.61hogging at d

The settlement of b and c turns the support moments into sagging moments. The result is symmetrical about the mid-point of bc, as the loading, rotations and settlements are.

Free body diagrams: shears and reactions

Span-wise (shear at left end, taking moments of each span):

  • ab: Va=32.58V_{a} = 32.58 kN up; after the 20 kN load V=12.58V = 12.58 kN; VbV_b(left) = 12.58 kN.
  • bc: VbV_b(right) = +5.00 kN, falling at 2 kN/m to −5.00-5.00 kN at c.
  • cd: VcV_c = -12.58 kN; after the 20 kN load -32.58 kN at d.

Reactions: Ra=32.58R_a = 32.58 kN up with Ma=62.61M_a = 62.61 kN·m anticlockwise; Rb=7.58R_b = 7.58 kN down; Rc=7.58R_c = 7.58 kN down; Rd=32.58R_d = 32.58 kN up with Md=62.61M_d = 62.61 kN·m clockwise. Check: 32.58+32.58−7.58−7.58=50=20+20+2×532.58 + 32.58 - 7.58 - 7.58 = 50 = 20+20+2\times5.

BMD and SFD values

SectionBM (kN·m)SF (kN)
a-62.61+32.58
2 m from a (load)+2.55+32.58 / +12.58
b+27.72+12.58 / +5.00
mid of bc (2.5 m)+33.970
c+27.72-5.00 / -12.58
2 m from d (load)+2.55-12.58 / -32.58
d-62.61-32.58

BMD is linear in ab and cd between the loads, parabolic in bc (M=27.72+5x−x2M = 27.72 + 5x - x^2, xx from b); SFD is stepped in ab and cd and a straight line through zero at mid-bc.

Answer: θb=0.001993\theta_b = 0.001993 rad, θc=−0.001993\theta_c = -0.001993 rad; Mab=−62.61M_{ab} = -62.61, Mba=−27.72M_{ba} = -27.72, Mbc=27.72M_{bc} = 27.72, Mcb=−27.72M_{cb} = -27.72, Mcd=27.72M_{cd} = 27.72, Mdc=62.61M_{dc} = 62.61 kN·m.

✓ Answer checked by Claude Opus 5.5 (high effort)

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