Statics: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

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1Formulas and methods

Vectors: dot & cross product

Magnitude
|a| = √(ax² + ay² + az²)
Unit vector
û = a/|a|
Components from an angle
Fx = F·cos θ, Fy = F·sin θ
Dot product
a·b = axbx + ayby + azbz = |a||b|cos θ
Scalar projection of a onto b
a·b/|b|
Work
W = F·d
Cross product
a × b = (aybz − azby, azbx − axbz, axby − aybx)
Areas
parallelogram |a × b|, triangle ½|a × b|
Moment about O
MO = r × F, r = A − O
Volume of a parallelepiped
V = |a·(b × c)|

Method

  1. Write every vector in components; for a force given by a magnitude and an angle, use F·cos θ and F·sin θ.
  2. For lengths and directions use the magnitude √(x² + y² + z²) and the unit vector a/|a|.
  3. Use the dot product for angles, projections, perpendicularity and work: a·b = |a||b|cos θ.
  4. Use the cross product for perpendicular vectors, areas and moments: write the three components carefully, keeping the order a × b.

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.

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.

Frames & machines

Equilibrium of each member
ΣFx = 0, ΣFy = 0, ΣM = 0
Two-force member
force along the line through its two pins
Pin force
equal and opposite on the two members it joins
Magnitude of a pin force
F = √(Fx² + Fy²)
Lever, pliers, bell crank
Fin·a = Fout·b
Toggle
Flink = F/(2 sin θ), Q = F/(2 tan θ)
Uniform load
resultant w·L at the middle of the load

Method

  1. Draw the whole structure and find the support reactions if there are no more than three unknowns.
  2. Spot the two-force members: loaded only at two pins, their force acts along the line between the pins.
  3. Take the frame apart and draw every member on its own, with equal and opposite pin forces where members meet.
  4. For each member, take moments about a pin with unknown forces, then use ΣFx = 0 and ΣFy = 0; combine components into a magnitude at the end.

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.

Centroid & second moment of area

Centroid
ȳ = ΣAiyi/ΣAi
Rectangle
I = bh³/12
Parallel-axis theorem
I = Ic + A·d²
Composite section
I = Σ(Ic,i + Aidi²)

2Practice problems

1.Vectors: dot & cross productMedium
xyzab

Find the dot product a·b of a = (7, 6, 7) and b = (2, −6, 4).

a = (7, 6, 7)b = (2, −6, 4)
a·b =
2.Vectors: dot & cross productHard
xyzab

The unit vector n̂ is perpendicular to both a = (−1, 4, 2) and b = (0, 2, −3) and has a positive z-component. Find its y-component n̂y.

a = (−1, 4, 2)b = (0, 2, −3)n̂z > 0
n̂y =
3.Beam support reactionsMedium
P1​ = 60 kNP2​ = 15 kNABRA​RB​ = ?2 m6 m2 m

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

L = 10 mP1 = 60 kN at 2 mP2 = 15 kN at 8 m
RB = kN
4.Beam support reactionsHard
P = 65 kNQ = 45 kNADCMA​ = ?0.5 m2 m1 m2.5 m

A compound beam is fixed to the wall at A, has an internal hinge at C (2.5 m from A) and rests on a roller at D (6 m from A). It carries a point load P at 3.5 m from A and a point load Q at 0.5 m from A. Find the magnitude of the reaction moment MA at the wall.

AC = 2.5 mAD = 6 mP = 65 kN at 3.5 mQ = 45 kN at 0.5 m
MA = kN·m
5.Truss: method of jointsMedium
ABBCACACB60 kN8 m5 m4 m

Use the method of joints to find the force FAB in member AB. Give tension as positive and compression as negative.

span = 8 mheight = 4 mB is 5 m from Avertical load = 60 kN
FAB = kN
6.Truss: method of jointsHard
ABCDEFGH10 kN10 kN30 kN30 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: 10 kN ↓F: 10 kN →G: 30 kN ↓H: 30 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
7.Frames & machinesMedium
5 kN3 m4 m0.45 mABCK

The frame shown has pins at A, B and C; A and C are fixed to the ground 3 m apart, and B is 4 m above the ground and 0.45 m to the right of A. A vertical load of 5 kN acts on member AB at K, 0.3375 m (horizontally) from A. Find the force FBC in member BC.

P = 5 kNL = 3 mH = 4 mhorizontal distance A to B = 0.45 mhorizontal distance A to K = 0.3375 m
FBC = kN
8.Frames & machinesHard
10 kN2 m1.5 m2.5 mABCDE

The A-frame shown stands on a pin at A and a roller at B, 2 m apart. The legs meet at the pin C, 4 m high, and are tied by the horizontal bar DE at 1.5 m. A horizontal force of 10 kN to the right acts at C. Find the tension T in the tie.

P = 10 kNAB = 2 mheight of C = 4 mheight of DE = 1.5 m
T = kN
9.Shear force & bending momentMedium
w = 10 kN/mABsection5 m3 m

Find the bending moment Mx at the section x = 5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mw = 10 kN/m from 0 to 8 mx = 5 m
Mx = kN·m
10.Shear force & bending momentHard
10 kN/m25 kN40 kNABCDEFG1 m1 m1 m1 m1 m1 m

The marks A to G split the beam into six equal parts. At which mark is the bending moment largest in size, sagging or hogging? Click it in the diagram.

25 kN @ 0 m40 kN @ 6 m10 kN/m, 1–4 m
  1. 1A (x = 0 m)
  2. 2B (x = 1 m)
  3. 3C (x = 2 m)
  4. 4D (x = 3 m)
  5. 5E (x = 4 m)
  6. 6F (x = 5 m)
  7. 7G (x = 6 m)
11.Centroid & second moment of areaMedium
1303801810xdimensions in mm

A symmetric I-section has flanges 130 mm wide and 18 mm thick, an overall depth of 380 mm and a web 10 mm thick. Find its second moment of area Ix about the horizontal centroidal axis x.

B = 130 mmH = 380 mmtf = 18 mmtw = 10 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
100251008xM = 10 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 10 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 100 mmtf = 25 mmtw = 8 mmhw = 100 mmM = 10 kN·m
σtop = MPa

3Solutions

1.Vectors: dot & cross product

Answer: a·b = 6

Dot product: a·b = axbx + ayby + azbz = |a|·|b|·cos θ, a scalar. It gives the angle between two vectors, cos θ = a·b/(|a|·|b|), and it is zero when they are perpendicular. The scalar projection of a onto b is a·b/|b|, and a constant force F moving through a displacement d does work W = F·d.

Multiply matching components and add

a·b = 7·2 + 6·(−6) + 7·4 = 14 + (−36) + 28 = 6

Answer

a·b = 6

Positive: the angle between the vectors is less than 90°.

2.Vectors: dot & cross product

Answer: n̂y = 0.1829

Cross product: a × b = (aybz − azby, azbx − axbz, axby − aybx) is perpendicular to both vectors, and |a × b| = |a|·|b|·sin θ is the area of the parallelogram they span (the triangle has half of it). Order matters: b × a = −(a × b). The moment of a force F applied at point A about point O is MO = r × F, with r = A − O.

Cross product

(a × b)x = aybz − azby = 4·(−3) − 2·2 = −16
(a × b)y = azbx − axbz = 2·0 − (−1)·(−3) = −3
(a × b)z = axby − aybx = (−1)·2 − 4·0 = −2

Normalise

The z-component of a × b is negative, so use −(a × b).

|a × b| = √((−16)² + (−3)² + (−2)²) = 16.4
n̂ = −(−16, −3, −2)/16.4 = (0.9755, 0.1829, 0.1219)
n̂y = 0.1829

Answer

n̂y = 0.1829
3.Beam support reactions

Answer: RB = 24 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​ = 60 kNP2​ = 15 kNABRA​RB​2 m6 m2 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·10 = 60·2 + 15·8
RB = 240/10 = 24 kN
ΣFy = 0: RA = 75 − 24 = 51 kN

Answer

RB = 24 kN
4.Beam support reactions

Answer: MA = 138.6 kN·m

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Replace each distributed load by its resultant (its area) acting at the centroid of the load diagram, and take moments about a support to remove that support’s reaction from the equation. An internal hinge cannot carry a bending moment, which gives one extra equation: the moment about the hinge of the forces on either side is zero.

Part CD

The hinge has no moment, so moments about C on CD alone must balance.

ΣMC = 0: RD·3.5 = 65·1
RD = 18.57 kN
VC = 65 − 18.57 = 46.43 kN

Part AC

The hinge force VC acts downward on AC (equal and opposite to its action on CD).

RA = 45 + 46.43 = 91.43 kN
MA = 45·0.5 + 46.43·2.5 = 138.6 kN·m

Answer

MA = 138.6 kN·m
5.Truss: method of joints

Answer: FAB = −36.02 kN

Method of joints: every pin of a truss is in equilibrium, so ΣFx = 0 and ΣFy = 0 at each joint. Start at a joint with at most two unknown member forces. A negative result means the member is in compression.

ABBCACACB60 kNAy​Cy​

Support reactions

Equilibrium of the whole truss. Moments about A, counter-clockwise positive.

ΣMA = 0: Cy·8 = 60·5 → Cy = 37.5 kN
ΣFy = 0: Ay = 60 − 37.5 = 22.5 kN

Joint A

Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.

sin α = 4/6.403 = 0.6247
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −22.5/0.6247 = −36.02 kN

Answer

FAB = −36.02 kN (compression)
6.Truss: method of joints

Answer: member DH

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 D

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

ΣF⊥ = 0 → FDH = 0

Check with the method of joints

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

AB: 47.5 kN (T), BC: 47.5 kN (T), CD: 55.83 kN (T), DE: 55.83 kN (T), FG: 71.67 kN (C), GH: 71.67 kN (C), AF: 46.88 kN (C), HE: 69.79 kN (C), BF: 10 kN (T), CG: 30 kN (C), DH: 0, FC: 30.21 kN (T), HC: 19.79 kN (T)

Answer

Zero-force member: DH
7.Frames & machines

Answer: FBC = 0.6671 kN

Frames and machines: unlike a truss, a frame contains at least one member that carries forces at more than two points, or a load between its pins. First look for two-force members: a member loaded only at two pins has its force along the line through them, so it adds one unknown, not two. Then use the whole structure for the support reactions when there are no more than three unknowns. Finally take the frame apart: draw each member separately, with the pin forces equal and opposite on the two members they connect, and write ΣFx = 0, ΣFy = 0 and ΣM = 0 for it. Taking moments about a pin removes both components of that pin force from the equation.

Two-force member BC

BC = √(2.55² + 4²) = 4.744 m

Whole frame: moments about A

The ground pushes on BC at C along CB; its horizontal component passes through A, only the vertical one has a moment.

FBC·(4/4.744)·3 = 5·0.3375
FBC = 0.6671 kN (compression)

Answer

FBC = 0.6671 kN
8.Frames & machines

Answer: T = 8 kN

Frames and machines: unlike a truss, a frame contains at least one member that carries forces at more than two points, or a load between its pins. First look for two-force members: a member loaded only at two pins has its force along the line through them, so it adds one unknown, not two. Then use the whole structure for the support reactions when there are no more than three unknowns. Finally take the frame apart: draw each member separately, with the pin forces equal and opposite on the two members they connect, and write ΣFx = 0, ΣFy = 0 and ΣM = 0 for it. Taking moments about a pin removes both components of that pin force from the equation.

Whole frame: moments about A

By·2 = 10·4
By = 20 kN

Leg BC: moments about C

20·1 = T·2.5
T = 8 kN

Answer

T = 8 kN

A positive T means the tie is in tension, as assumed.

9.Shear force & bending moment

Answer: Mx = 75 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 = 10·8 = 80 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 10·8·4
RB = 320/8 = 40 kN
ΣFy = 0: RA = 80 − 40 = 40 kN
w = 10 kN/mABRA​ = 40RB​ = 40section5 m3 m

Cut at x = 5 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 = 40·5 − 10·5·2.5 = 75 kN·m

Answer

Mx = 75 kN·m
10.Shear force & bending moment

Answer: E (x = 4 m)

Largest bending moment: M changes slope wherever the shear force changes, so its peaks sit where the shear force crosses zero: under a point load, inside a distributed load, or over a support of an overhang. At a fixed support of a cantilever the moment is largest at the wall. Compare the size of M at those places, sagging or hogging.

Support reactions

Take moments about one support, then use the vertical force balance.

R1 = 21.67 kN, R2 = 73.33 kN

Bending moment at every mark

Sum the moments of all forces on one side of the cut. Sagging is positive, hogging negative.

MA = 0, MB = −25, MC = −33.33, MD = −51.67, ME = −80 kN·m, MF = −40, MG = 0

Answer

Mark E: ME = −80 kN·m
11.Centroid & second moment of area

Answer: Ix = 187.4 × 10⁶ mm⁴

Second moment of area: for a rectangle about its own centroidal axis I = bh³/12, and about its base bh³/3 (parallel-axis theorem I = Ic + A·d²). A hole is handled by subtracting its I, as long as both parts share the same axis. The elastic section modulus is S = I/c, where c is the distance to the extreme fibre.

Outer rectangle minus the two side cut-outs

Both cut-outs together are (B − tw) wide and hw = H − 2tf high, and share the axis x.

hw = 380 − 2·18 = 344 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (130·380³ − 120·344³)/12
Ix = 1.874 × 10⁸ mm⁴ = 187.4 × 10⁶ mm⁴

Answer

Ix = 187.4 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 87.39 MPa

Composite areas: split the section into rectangles. The centroid is the area-weighted average ȳ = ΣAᵢyᵢ/ΣAᵢ. The second moment of area about the centroidal axis adds each part’s own bh³/12 and its parallel-axis term A·d², where d is the distance from the part’s centroid to the overall centroid. Bending stress is σ = M·y/I.

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 100·25 = 2500 mm², yf = 100 + 25/2 = 112.5 mm
web: Aw = 8·100 = 800 mm², yw = 100/2 = 50 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2500·112.5 + 800·50)/3300 = 97.35 mm

Parallel-axis theorem

flange: 100·25³/12 + 2500·(112.5 − 97.35)² = 704129 mm⁴
web: 8·100³/12 + 800·(50 − 97.35)² = 2.46 × 10⁶ mm⁴
Ix = 704129 + 2.46 × 10⁶ = 3.164 × 10⁶ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 125 − 97.35 = 27.65 mm
σ = M·y/I = 1 × 10⁷·27.65/3.164 × 10⁶ = 87.39 MPa

Answer

σtop = 87.39 MPa

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