Skip to main content

Stepped bar displacements and support forces

Short answer

Use four bar elements of length l/4 with areas A, 1.5A, 0.5A, 0.75A and fixed ends. Nodal displacements are u2=Pl/(5AE), u3=Pl/(6AE), u4=Pl/(15AE). Support reactions are 0.8P and 0.2P, both opposite to the applied load.

For the given stepped bar obtain the nodal displacements at nodes 2, 3 and 4. Also obtain the forces developed at the supports. Take EE = constant and cross-sectional areas as indicated in the figure.

[Figure: bar fixed at both ends (nodes 1 and 5), four equal elements each of length l/4l/4 between nodes 1-2-3-4-5; cross-sectional areas AA (element 1), 3A/23A/2 (element 2), A/2A/2 (element 3), 3A/43A/4 (element 4); a point load PP acts at node 2 in the +x direction]

Take k=AE/lk=AE/l as the unit of stiffness. Each element has length l/4l/4, so ke=AeE/(l/4)=4AeE/lk_e = A_eE/(l/4)=4A_eE/l.

Element stiffnesses

ElementNodesAreakek_e
11-2AA4k4k
22-33A/23A/26k6k
33-4A/2A/22k2k
44-53A/43A/43k3k

Each element matrix is ke[1−1−11]k_e\begin{bmatrix}1&-1\\-1&1\end{bmatrix}.

Assembled global equations

k[4−4000−410−6000−68−2000−25−3000−33][u1u2u3u4u5]=[R1P00R5]k\begin{bmatrix}4&-4&0&0&0\\-4&10&-6&0&0\\0&-6&8&-2&0\\0&0&-2&5&-3\\0&0&0&-3&3\end{bmatrix}\begin{bmatrix}u_1\\u_2\\u_3\\u_4\\u_5\end{bmatrix}=\begin{bmatrix}R_1\\P\\0\\0\\R_5\end{bmatrix}

Boundary conditions: u1=u5=0u_1=u_5=0

Deleting rows and columns 1 and 5:

AEl[10−60−68−20−25][u2u3u4]=[P00]\frac{AE}{l}\begin{bmatrix}10&-6&0\\-6&8&-2\\0&-2&5\end{bmatrix}\begin{bmatrix}u_2\\u_3\\u_4\end{bmatrix}=\begin{bmatrix}P\\0\\0\end{bmatrix}

From row 3: u4=0.4u3u_4=0.4u_3. Row 2: −6u2+8u3−2(0.4u3)=0⇒u3=67.2u2=56u2-6u_2+8u_3-2(0.4u_3)=0\Rightarrow u_3=\dfrac{6}{7.2}u_2=\dfrac{5}{6}u_2. Row 1: 10u2−6⋅56u2=5u2=PlAE10u_2-6\cdot\dfrac56u_2=5u_2=\dfrac{Pl}{AE}.

u2=Pl5AE,u3=Pl6AE,u4=Pl15AEu_2=\frac{Pl}{5AE},\qquad u_3=\frac{Pl}{6AE},\qquad u_4=\frac{Pl}{15AE}

Support reactions

R1=4k(u1−u2)=−4P5=−0.8P,R5=3k(u5−u4)=−P5=−0.2PR_1=4k(u_1-u_2)=-\frac{4P}{5}=-0.8P,\qquad R_5=3k(u_5-u_4)=-\frac{P}{5}=-0.2P

Both act in the −x-x direction (towards the left). Check: P−0.8P−0.2P=0P-0.8P-0.2P=0.

Element forces (check)

F1=k1(u2−u1)=+0.8PF_1=k_1(u_2-u_1)=+0.8P (tension); F2=6k(u3−u2)=−0.2PF_2=6k(u_3-u_2)=-0.2P; F3=2k(u4−u3)=−0.2PF_3=2k(u_4-u_3)=-0.2P; F4=3k(u5−u4)=−0.2PF_4=3k(u_5-u_4)=-0.2P (compression). Equilibrium at node 2: P−0.8P−0.2P=0P-0.8P-0.2P=0.

Answer: u2=Pl5AE, u3=Pl6AE, u4=Pl15AEu_2=\dfrac{Pl}{5AE},\ u_3=\dfrac{Pl}{6AE},\ u_4=\dfrac{Pl}{15AE}; R1=0.8PR_1=0.8P and R5=0.2PR_5=0.2P, both acting opposite to PP.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Computational Techniques in Civil Engineering chapter 4 questions →