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Chapter 2 · 2 hours

Mathematical Background

Practice questions

Practice questions and answers

2 exam-style questions on this chapter, written for this site from the official syllabus. We haven’t found past IOE papers for this subject yet; if you have some, share them in the community.

  • Practice · 6 marks

A three-degree-of-freedom structure has the stiffness matrix (in kN/mm)
[K]=[5−20−24−10−13][K] = \begin{bmatrix} 5 & -2 & 0 \\ -2 & 4 & -1 \\ 0 & -1 & 3 \end{bmatrix} and load vector {F}={10, 0, 6}T\{F\} = \{10,\ 0,\ 6\}^T kN. (a) Show that [K][K] is symmetric and positive definite. (b) Solve [K]{u}={F}[K]\{u\} = \{F\} by Gauss elimination and state the displacements in mm. Why must a stiffness matrix be positive definite after boundary conditions are applied?

Answer

(a) Symmetry and positive definiteness

K12=K21=−2K_{12} = K_{21} = -2, K23=K32=−1K_{23} = K_{32} = -1, K13=K31=0K_{13} = K_{31} = 0, so [K][K] is symmetric.

For positive definiteness, all leading principal minors must be positive:

  • Δ1=5>0\Delta_1 = 5 > 0
  • Δ2=5(4)−(−2)(−2)=16>0\Delta_2 = 5(4) - (-2)(-2) = 16 > 0
  • Δ3=det⁡[K]=5(12−1)+2(−6−0)=55−12=43>0\Delta_3 = \det[K] = 5(12-1) + 2(-6-0) = 55 - 12 = 43 > 0

All are positive, so [K][K] is positive definite and a unique solution exists.

(b) Gauss elimination

Augmented matrix:

[5−2010−24−100−136]\left[\begin{array}{ccc|c} 5 & -2 & 0 & 10 \\ -2 & 4 & -1 & 0 \\ 0 & -1 & 3 & 6 \end{array}\right]

Step 1: R2←R2+0.4R1R_2 \leftarrow R_2 + 0.4R_1 gives [0, 3.2, −1 ∣ 4][0,\ 3.2,\ -1\,|\,4].

Step 2: R3←R3+13.2R2=R3+0.3125R2R_3 \leftarrow R_3 + \frac{1}{3.2}R_2 = R_3 + 0.3125R_2 gives [0, 0, 2.6875 ∣ 7.25][0,\ 0,\ 2.6875\,|\,7.25].

Back substitution:

u3=7.252.6875=2.698 mmu2=4+2.6983.2=2.093 mmu1=10+2(2.093)5=2.837 mm\begin{aligned} u_3 &= \frac{7.25}{2.6875} = 2.698\ \text{mm} \\ u_2 &= \frac{4 + 2.698}{3.2} = 2.093\ \text{mm} \\ u_1 &= \frac{10 + 2(2.093)}{5} = 2.837\ \text{mm} \end{aligned}

Check: row 3 gives −2.093+3(2.698)=6.00-2.093 + 3(2.698) = 6.00 kN. Also the product of pivots 5×3.2×2.6875=43=det⁡[K]5 \times 3.2 \times 2.6875 = 43 = \det[K].

Why positive definite: strain energy U=12{u}T[K]{u}U = \tfrac{1}{2}\{u\}^T[K]\{u\} must be positive for every non-zero displacement. If a rigid-body motion remains (supports missing), [K][K] is singular and the equations cannot be solved. Positive pivots also guarantee that elimination runs without row interchange.

Answer: u1=2.837u_1 = 2.837 mm, u2=2.093u_2 = 2.093 mm, u3=2.698u_3 = 2.698 mm.

  • Practice · 4 marks

Differentiate between essential (geometric) and natural (force) boundary conditions with examples. Classify the differential equation EI d4wdx4=qEI\,\dfrac{d^4 w}{dx^4} = q and state the boundary conditions of a cantilever beam of length LL in terms of ww.

Answer

Differences

PointEssential (geometric) BCNatural (force) BC
SpecifiesValue of the primary variable (uu, ww, θ\theta, TT)Value of the secondary variable (force, moment, flux)
Order of derivativeLower, up to (m−1)(m-1) for order 2m2mHigher, mm and above
Example, baru(0)=0u(0) = 0 at fixed endAE u′(L)=PAE\,u'(L) = P at loaded end
In weak formMust be satisfied by the trial functionAppears in the weak form and is satisfied automatically
In FEMApplied by deleting or modifying rowsAdded to the load vector

Classification

EI w′′′′=qEI\,w'''' = q is a linear, fourth-order, ordinary differential equation (one independent variable xx). For a fourth-order equation m=2m = 2, so ww and w′w' are primary variables (essential), while EIw′′EIw'' (moment) and EIw′′′EIw''' (shear) are secondary variables (natural).

Cantilever beam (fixed at x=0x=0, free at x=Lx=L)

  • Essential: w(0)=0w(0) = 0, dwdx(0)=0\dfrac{dw}{dx}(0) = 0
  • Natural: EId2wdx2(L)=0EI\dfrac{d^2w}{dx^2}(L) = 0 (zero moment), EId3wdx3(L)=0EI\dfrac{d^3w}{dx^3}(L) = 0 (zero shear)

Written from the official syllabus. Questions and answers are written for this site; check them against your class notes.

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