Structural Analysis: cram pack

Formula sheets, the key method steps for every topic and 10 practice problems, with full solutions at the back.

New problemsBack to the course

In the print window, choose “Save as PDF” to keep a copy on your device.

1Formulas and methods

Beam support reactions

Equilibrium
ΣFx = 0, ΣFy = 0, ΣM = 0
Uniform load
resultant w·L at the middle of the load
Moment
M = F·d

Method

  1. Draw a free-body diagram and replace each support by its reactions.
  2. Replace every distributed load by a single force at its centroid.
  3. Take moments about one support to find the reaction at the other.
  4. Use ΣFy = 0 to find the remaining reaction, and check with a second moment equation.

Shear force & bending moment

Shear and moment
V = ΣF on one side, M = ΣF·d on one side
Bending stress
σ = M·y/I
Rectangle
I = bh³/12
Section modulus
W = I/ymax
Simply supported, uniform load
Mmax = wL²/8

Method

  1. Find the support reactions from equilibrium of the whole beam.
  2. Cut the beam at the section you need and keep one side.
  3. Shear force: sum of the vertical forces on that side. Bending moment: sum of their moments about the cut.
  4. For the maximum moment, find where the shear force is zero.

Truss: method of joints

Method of joints
ΣFx = 0, ΣFy = 0 at each joint
Method of sections
ΣM = 0 about a cut point
Member force
positive = tension, negative = compression

Method

  1. Find the support reactions for the whole truss.
  2. Method of joints: start at a joint with at most two unknown member forces and use ΣFx = 0 and ΣFy = 0.
  3. Method of sections: cut through the member you need and take moments about a point where the other unknown members meet.
  4. Assume tension; a negative answer means compression.

Beam deflection

Point load at midspan
δ = PL³/(48EI)
Uniform load, simply supported
δ = 5wL⁴/(384EI)
Cantilever, end load
δ = PL³/(3EI)
Cantilever, uniform load
δ = wL⁴/(8EI)
Superposition
δ = δ1 + δ2

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

2Practice problems

1.Beam support reactionsMedium
P1​ = 20 kNP2​ = 30 kNABRA​RB​ = ?1 m1.5 m1.5 m

The simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RB.

L = 4 mP1 = 20 kN at 1 mP2 = 30 kN at 2.5 m
RB = kN
2.Beam support reactionsHard
w = 6 kN/mP = 60 kNABRA​RB​ = ?1 m2 m1 m1 m

The simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RB.

L = 5 mP = 60 kN at 3 mw = 6 kN/m from 1 to 4 m
RB = kN
3.Shear force & bending momentMedium
w = 4 kN/mABsection2 m8 m

Find the bending moment Mx at the section x = 2 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mw = 4 kN/m from 0 to 10 mx = 2 m
Mx = kN·m
4.Shear force & bending momentHard
w = 5 kN/mP = 15 kNABsection2 m6 m

Find the bending moment Mx at the section x = 2 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 15 kN at 2 mw = 5 kN/m from 0 to 8 mx = 2 m
Mx = kN·m
5.Truss: method of jointsMedium
ABCDEFGH30 kN10 kN25 kN4 × 4 m3 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

B: 30 kN ↓C: 10 kN ↓D: 25 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member FC
  13. 13member HC
6.Truss: method of jointsHard
ABCDEFGH25 kN4 × 3 m4 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

H: 25 kN ←
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member BG
  13. 13member DG
7.Beam deflectionMedium
w = 10 kN/mδL = 4 m

A simply supported beam carries a uniformly distributed load w over its whole span. Find the maximum deflection δmax, at midspan.

w = 10 kN/mL = 4 mE = 200 GPa (steel)I = 8.5 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
P = 65 kNAB2 m2 m

A propped cantilever is fixed at A and simply supported (propped) at B. It carries a point load P at midspan. EI is constant. Find the reaction RB at the prop.

L = 4 mP = 65 kN at 2 m
RB = kN
9.Column bucklingMedium
PL = 5 m20 × 60 mmcross-section

A column of length L made of steel is fixed at both ends. Using Euler’s formula, find its critical buckling load Pcr.

L = 5 mE = 200 GPa (steel)b × h = 20 × 60 mm
Pcr = kN
10.Column bucklingHard
P = 90 kNL = 5 md = ?cross-section

A solid round column of length L made of aluminium is fixed at the base and free at the top. It must carry 90 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 90 kNn = 2.5L = 5 mE = 70 GPa (aluminium)
d = mm

3Solutions

1.Beam support reactions

Answer: RB = 23.75 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Taking moments about one support removes that support’s reaction from the equation.

P1​ = 20 kNP2​ = 30 kNABRA​RB​1 m1.5 m1.5 m

Free-body diagram

Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.

Equilibrium

Moments about A, counter-clockwise positive. Then vertical force balance.

ΣMA = 0: RB·4 = 20·1 + 30·2.5
RB = 95/4 = 23.75 kN
ΣFy = 0: RA = 50 − 23.75 = 26.25 kN

Answer

RB = 23.75 kN
2.Beam support reactions

Answer: RB = 45 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Taking moments about one support removes that support’s reaction from the equation.

w = 6 kN/mP = 60 kNABRA​RB​1 m2 m1 m1 m

Free-body diagram

Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.

Equilibrium

Moments about A, counter-clockwise positive. Then vertical force balance.

UDL resultant: W = w·ℓ = 6·3 = 18 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 60·3 + 6·3·2.5
RB = 225/5 = 45 kN
ΣFy = 0: RA = 78 − 45 = 33 kN

Answer

RB = 45 kN
3.Shear force & bending moment

Answer: Mx = 32 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 4·10 = 40 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 4·10·5
RB = 200/10 = 20 kN
ΣFy = 0: RA = 40 − 20 = 20 kN
w = 4 kN/mABRA​ = 20RB​ = 20section2 m8 m

Cut at x = 2 m and keep the left part

Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 20·2 − 4·2·1 = 32 kN·m

Answer

Mx = 32 kN·m
4.Shear force & bending moment

Answer: Mx = 52.5 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 5·8 = 40 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 15·2 + 5·8·4
RB = 190/8 = 23.75 kN
ΣFy = 0: RA = 55 − 23.75 = 31.25 kN
w = 5 kN/mP = 15 kNABRA​ = 31.25RB​ = 23.75section2 m6 m

Cut at x = 2 m and keep the left part

Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 31.25·2 − 5·2·1 = 52.5 kN·m

Answer

Mx = 52.5 kN·m
5.Truss: method of joints

Answer: member CG

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint G

FG and GH lie on one straight line and the joint carries no load. Balancing forces across that line leaves only CG.

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

Solving all joints gives these member forces (T = tension, C = compression).

AB: 45 kN (T), BC: 45 kN (T), CD: 41.67 kN (T), DE: 41.67 kN (T), FG: 50 kN (C), GH: 50 kN (C), AF: 56.25 kN (C), HE: 52.08 kN (C), BF: 30 kN (T), CG: 0, DH: 25 kN (T), FC: 6.25 kN (T), HC: 10.42 kN (T)

Answer

Zero-force member: CG
6.Truss: method of joints

Answer: member CG

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint C

BC and CD lie on one straight line and the joint carries no load. Balancing forces across that line leaves only CG.

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

Solving all joints gives these member forces (T = tension, C = compression).

AB: 18.75 kN (C), BC: 12.5 kN (C), CD: 12.5 kN (C), DE: 6.25 kN (C), FG: 6.25 kN (C), GH: 18.75 kN (C), AF: 10.42 kN (C), HE: 10.42 kN (T), BF: 8.333 kN (T), CG: 0, DH: 8.333 kN (C), BG: 10.42 kN (C), DG: 10.42 kN (T)

Answer

Zero-force member: CG
7.Beam deflection

Answer: δmax = 19.61 mm

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition).

Consistent units

Work in N and mm: P in N, w in N/mm (kN/m = N/mm), L in mm, E in N/mm² (GPa × 1000), I in mm⁴.

w = 10 N/mm, L = 4000 mm
EI = 1.7 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·10·4000⁴/(384·1.7 × 10¹²) = 19.61 mm

Answer

δmax = 19.61 mm
8.Beam deflection

Answer: RB = 20.31 kN

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition). For a statically indeterminate beam, remove a redundant support and require the deflection there to be zero (compatibility).

Remove the prop

Without the prop the beam is a cantilever. Its free end would deflect under the load.

δload = P(L/2)²(3L − L/2)/(6EI) = 5PL³/(48EI)

Compatibility at the prop

The prop force RB alone lifts the free end by RBL³/(3EI). The prop holds B at zero deflection, so the two must cancel. EI cancels out.

RB·L³/(3EI) = 5PL³/(48EI) → RB = 5P/16 = 5·65/16 = 20.31 kN

Answer

RB = 20.31 kN
9.Column buckling

Answer: Pcr = 12.63 kN

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Smallest second moment of area

A rectangle buckles about its weak axis, using the smaller dimension cubed.

Imin = h·b³/12 = 60·20³/12 = 40000 mm⁴

Effective length

KL = 0.5·5000 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·40000/2500² = 12633 N = 12.63 kN

Answer

Pcr = 12.63 kN
10.Column buckling

Answer: d = 160.5 mm

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Required critical load

Pcr = n·P = 2.5·90000 = 225000 N
KL = 2·5000 = 10000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·225000·10000²/(π³·70000))^(1/4) = 160.5 mm

Answer

d = 160.5 mm

Check: the slenderness KL/r is 249.2, so the column is slender and Euler applies.

ExamProblems · examproblems.com/courses/structural-analysis