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Flexibility matrix: reactions at support D

Short answer

Remove the hinge at D; treat the frame as a cantilever fixed at A. Compute moment diagrams for unit loads at D and for applied loads, form the flexibility matrix, calculate load displacements, and solve [F]{R} = -{Δ}. Vertical reaction at D = 5.95 kN upward, horizontal = 2.07 kN to the left.

Generate the flexibility matrix for the coordinates shown in figure below and use this to determine the reactions at support D. Take EI is constant for all members. [Figure: portal frame ABCD, height 5 m, span 4 m; A fixed, D hinged; 2 kN/m UDL on the left column AB (printed near B) and a 5 kN horizontal load at C; coordinates 1 (vertical) and 2 (horizontal) at D.]

Assumptions: A is fixed, D is hinged. AB = CD = 5 m high, BC = 4 m, EI constant. The 2 kN/m UDL acts horizontally (to the right) on AB and the 5 kN load acts to the right at C. Axial deformations are ignored. The hinge D gives two unknown reactions, so the frame is indeterminate to the 2nd degree. The redundants are the coordinates at D: 1 = vertical reaction (up +) and 2 = horizontal reaction (right +).

Step 1: Released structure

Remove the hinge at D. The frame A-B-C-D becomes a cantilever fixed at A with a free end D.

Step 2: Moment diagrams (positive = tension on the inside face)

Caseon AB (A to B)on BC (B to C)on CD (C to D)
Unit vertical force at D (m1m_1)4 (constant)4 at B to 0 at C0
Unit horizontal force at D (m2m_2)0 at A to 5 at B5 (constant)5 at C to 0 at D
Given loads (MLM_L)-50 at A to 0 at B (parabolic)00

For the loaded case, ML=−[(5−y)2+5(5−y)]M_L=-\left[(5-y)^2+5(5-y)\right] on AB (y up from A): the UDL gives 2(5−y)2/22(5-y)^2/2 and the 5 kN load at C gives 5(5−y)5(5-y), both causing tension on the outside.

Step 3: Flexibility matrix (fij=∑∫mimj dx/EIf_{ij}=\sum\int m_im_j\,dx/EI)

f11=1EI[42(5)+42(4)3]=101.33EI,f22=1EI[533+52(4)+533]=183.33EIf_{11}=\frac{1}{EI}\left[4^2(5)+\frac{4^2(4)}{3}\right]=\frac{101.33}{EI},\quad f_{22}=\frac{1}{EI}\left[\frac{5^3}{3}+5^2(4)+\frac{5^3}{3}\right]=\frac{183.33}{EI} f12=f21=1EI[4⋅522+5⋅4×42]=90.00EIf_{12}=f_{21}=\frac{1}{EI}\left[4\cdot\frac{5^2}{2}+5\cdot\frac{4\times4}{2}\right]=\frac{90.00}{EI} [F]=1EI[101.3390.0090.00183.33][F]=\frac{1}{EI}\begin{bmatrix}101.33&90.00\\90.00&183.33\end{bmatrix}

Step 4: Displacements of D in the released structure due to the loads

Δ1L=1EI∫m1ML dx=−416.67/EI,Δ2L=1EI∫m2ML dx=−156.25/EI\Delta_{1L}=\frac{1}{EI}\int m_1M_L\,dx=-416.67/EI,\qquad \Delta_{2L}=\frac{1}{EI}\int m_2M_L\,dx=-156.25/EI

(negative: D moves down and to the left in the released frame.)

Step 5: Compatibility (D cannot move)

[F]{R1R2}=−{Δ1LΔ2L}  ⇒  {R1R2}={5.95−2.07} kN[F]\begin{Bmatrix}R_1\\R_2\end{Bmatrix}=-\begin{Bmatrix}\Delta_{1L}\\\Delta_{2L}\end{Bmatrix} \;\Rightarrow\; \begin{Bmatrix}R_1\\R_2\end{Bmatrix}=\begin{Bmatrix}5.95\\-2.07\end{Bmatrix}\ \text{kN}

Reactions at A (equilibrium)

HA=−(2×5+5)−(−2.07)=−12.93H_A=-(2\times5+5)-(-2.07)=-12.93 kN (to the left), VA=−5.95V_A=-5.95 kN, MA=26.21M_A=26.21 kNm. Check ∑Fx\sum F_x: loads 1515 kN to the right, reactions -12.93 and -2.07 kN, total =0=0 ✓.

Final BM (inside tension +): MA=−26.21M_A=-26.21, MB=13.45M_B=13.45, MC=−10.34M_C=-10.34, MD=0M_D=0 kNm.

Answer: reactions at D: vertical R1=5.95R_1=5.95 kN upward and horizontal R2=2.07R_2=2.07 kN directed to the left.

✓ Answer checked by Claude Opus 5.5 (high effort)

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