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Consistent deformation: frame, BMD, SFD, normal thrust

Short answer

Release fixed D and impose zero displacements there. Results: H_D=2.40 kN left, V_D=1.84 kN up, M_D=3.83 kNm anticlockwise; moments M_A=-4.90, M_B=-1.33, M_C=-3.38 kNm; axial compressions are AB 1.16, BC 2.40, CD 1.84 kN.

Use the consistent deformation method to solve the frame and draw bending moment, shear force and normal thrust diagrams. [Figure: frame; left column (2I) of 6 m, fixed base, carrying 1 kN/m UDL horizontally; beam (2I) of 6 m with 3 kN at 3 m from the left; right column (I) of 3 m, fixed base.]

Assumptions: A(0,0) and D are fixed bases. Column AB (2I) is 6 m high, beam BC (2I) is 6 m and column CD (I) is 3 m high, so D is 3 m above the level of A. The 1 kN/m UDL acts horizontally to the right on AB; the 3 kN load acts downward at 3 m from B on BC. Axial deformation is ignored. Positive bending moment = tension on the inside of the frame.

Degree of indeterminacy

Reactions: 3 + 3 = 6; equations = 3, so Ds=3D_s=3. Release the fixed support D. The redundants are X1=HDX_1=H_D (right +), X2=VDX_2=V_D (up +) and X3=MDX_3=M_D (anticlockwise +). The primary structure is a cantilever fixed at A.

Moments in the primary structure (kNm; m1,m2,m3m_1,m_2,m_3 for unit X1,X2,X3X_1,X_2,X_3)

Sectionm1m_1 (H=1)m2m_2 (V=1)m3m_3 (M=1)MLM_L
A (AB)-3.006.001.00-27.00
B (AB)3.006.001.00-9.00
B (BC)3.006.001.00-9.00
C (BC)3.000.001.000.00
C (CD)3.000.001.000.00
D (CD)0.000.001.000.00

Flexibility matrix and load displacements (∫mimj ds/EI\int m_im_j\,ds/EI)

[F]=1EI[45.0027.0013.5027.00144.0027.0013.5027.009.00],{ΔL}=1EI{6.75−303.75−51.75}[F]=\frac{1}{EI}\begin{bmatrix}45.00&27.00&13.50\\27.00&144.00&27.00\\13.50&27.00&9.00\end{bmatrix},\qquad \{\Delta_L\}=\frac{1}{EI}\begin{Bmatrix}6.75\\-303.75\\-51.75\end{Bmatrix}

(For example f33=∑LEI=62+62+31=9f_{33}=\sum \dfrac{L}{EI}=\dfrac{6}{2}+\dfrac{6}{2}+\dfrac{3}{1}=9.)

Consistent deformation (D is fixed: all three displacements are zero)

[F]{X}=−{ΔL}  ⇒  X1=−2.404 kN,X2=1.842 kN,X3=3.831 kNm[F]\{X\}=-\{\Delta_L\}\;\Rightarrow\; X_1=-2.404\ \text{kN},\quad X_2=1.842\ \text{kN},\quad X_3=3.831\ \text{kNm}

So HD=2.40H_D=2.40 kN to the left, VD=1.84V_D=1.84 kN upward, MD=3.83M_D=3.83 kNm anticlockwise.

Reactions at A (equilibrium)

HA=6−2.40=3.60H_A=6-2.40=3.60 kN (left), VA=3−1.84=1.16V_A=3-1.84=1.16 kN (up), MA=4.90M_A=4.90 kNm (anticlockwise). Check: ∑Fx=6−3.60−2.40=0\sum F_x=6-3.60-2.40=0 ✓, ∑Fy=3−1.16−1.84=0\sum F_y=3-1.16-1.84=0 ✓.

Bending moment diagram (M=ML+∑XimiM=M_L+\sum X_im_i, kNm; + inside tension)

SectionBM
A-4.90
Mid-height of AB (3 m)1.38
B-1.33
Under 3 kN load (BC)2.14
C-3.38
D3.83

AB bends in a parabola (UDL); BC is two straight lines with a peak under the load; CD is a straight line with a change of sign.

Shear force and normal thrust

MemberAxial N (+ tension)Shear at startShear at end
AB-1.163.60-2.40
BC-2.401.16-1.84
CD-1.842.402.40

Shear sign: positive when the force on the start end of the member acts along its local y-axis (90° anticlockwise from the direction A to B, B to C, C to D). Axial: negative = compression. Normal thrust in AB, BC, CD is therefore 1.16, 2.40 and 1.84 kN compression. The shear in AB goes from 3.60 kN at A to -2.40 kN at B (linear, due to the UDL), and in BC it is 1.16 kN before the 3 kN load and -1.84 kN after it.

Answer: HD=2.40H_D=2.40 kN, VD=1.84V_D=1.84 kN, MD=3.83M_D=3.83 kNm; MA=−4.90M_A=-4.90, MB=−1.33M_B=-1.33, MC=−3.38M_C=-3.38 kNm (inside tension +).

✓ Answer checked by Claude Opus 5.5 (high effort)

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