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
xyzdFAB

A constant force F = (25, −20, −30) N acts on an object while it moves in a straight line from point A(−5, −3, 1) to point B(−1, −5, 3). Coordinates are in metres. Find the work W done by the force.

F = (25, −20, −30) NA(−5, −3, 1) mB(−1, −5, 3) m
W = J
2.Vectors: dot & cross productHard
xyzab

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

a = (−2, 3, −1)b = (4, 2, 0)n̂z > 0
n̂x =
3.Beam support reactionsMedium
w = 8 kN/mP = 60 kNABMA​ = ?4 m1 m5 m

The cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w from the wall to 4 m and a point load P at 5 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 10 mP = 60 kN at 5 mw = 8 kN/m from 0 to 4 m
MA = kN·m
4.Beam support reactionsHard
w = 12 kN/mP = 20 kNABRA​ = ?RB​3 m1 m6 m

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

L = 10 mP = 20 kN at 3 mw = 12 kN/m from 3 to 4 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB20 kN6 m1 m4 m

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

span = 6 mheight = 4 mB is 1 m from Avertical load = 20 kN
FBC = kN
6.Truss: method of jointsHard
ABCDEFGH10 kN35 kN15 kN4 × 3 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.

D: 10 kN ↓F: 35 kN →G: 15 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
12 kN6 m2.5 m3.6 mABCK

The frame shown has pins at A, B and C; A and C are fixed to the ground 6 m apart, and B is 2.5 m above the ground and 3.6 m to the right of A. A vertical load of 12 kN acts on member AB at K, 2.7 m (horizontally) from A. Find the force FBC in member BC.

P = 12 kNL = 6 mH = 2.5 mhorizontal distance A to B = 3.6 mhorizontal distance A to K = 2.7 m
FBC = kN
8.Frames & machinesHard
8 kN1.5 kN4 m3 mABC

A uniform horizontal boom AB of weight 1.5 kN is pinned to a wall at A and held by a cable from B to the point C on the wall, 3 m above A. A load of 8 kN hangs at B. Find the magnitude of the pin reaction A.

W = 8 kNWb = 1.5 kNAB = 4 mAC = 3 m
A = kN
9.Shear force & bending momentMedium
4 kN/m50 kNABCDEFG2 m2 m2 m2 m2 m2 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.

50 kN @ 4 m4 kN/m, 0–12 m
  1. 1A (x = 0 m)
  2. 2B (x = 2 m)
  3. 3C (x = 4 m)
  4. 4D (x = 6 m)
  5. 5E (x = 8 m)
  6. 6F (x = 10 m)
  7. 7G (x = 12 m)
10.Shear force & bending momentHard
w = 16 kN/mAB5 m1 m

The simply supported beam carries a uniformly distributed load over part of its span. Find the maximum bending moment Mmax in the beam.

L = 6 mw = 16 kN/m from 0 to 5 m
Mmax = kN·m
11.Centroid & second moment of areaMedium
180120t = 16xdimensions in mm

A channel section lies with its open side up: a base plate 180 mm wide with two upright legs, 120 mm high overall. Base and legs are all 16 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.

b = 180 mmh = 120 mmt = 16 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2603026020xM = 50 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 50 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 260 mmtf = 30 mmtw = 20 mmhw = 260 mmM = 50 kN·m
σtop = MPa

3Solutions

1.Vectors: dot & cross product

Answer: W = 80 J

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.

Displacement

d = B − A = (−1, −5, 3) − (−5, −3, 1) = (4, −2, 2) m

Work

W = F·d = 25·4 + (−20)·(−2) + (−30)·2 = 80 J

Answer

W = 80 J
2.Vectors: dot & cross product

Answer: n̂x = −0.1204

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

Normalise

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

|a × b| = √(2² + (−4)² + (−16)²) = 16.61
n̂ = −(2, −4, −16)/16.61 = (−0.1204, 0.2408, 0.9631)
n̂x = −0.1204

Answer

n̂x = −0.1204
3.Beam support reactions

Answer: MA = 364 kN·m

Cantilever equilibrium: a fixed support can push up and also resist rotation, so it gives a vertical reaction RA and a reaction moment MA. ΣFy = 0 gives RA, and moments about the wall give MA = Σ(load × distance from the wall). A distributed load acts as its resultant at the centroid of the load diagram.

Resultant of the distributed load

W = 8·4 = 32 kN, x̄ = 2 m

Moment about the wall

MA = P·a + W·x̄ = 60·5 + 32·2 = 364 kN·m

Answer

MA = 364 kN·m
4.Beam support reactions

Answer: RA = 21.8 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 = 12 kN/mP = 20 kNABRA​RB​3 m1 m6 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 = 12·1 = 12 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·10 = 20·3 + 12·1·3.5
RB = 102/10 = 10.2 kN
ΣFy = 0: RA = 32 − 10.2 = 21.8 kN

Answer

RA = 21.8 kN
5.Truss: method of joints

Answer: FBC = −5.336 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.

ABBCACACB20 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 20·1 → Cy = 3.333 kN
ΣFy = 0: Ay = 20 − 3.333 = 16.67 kN

Joint C

The roller gives only a vertical reaction, so joint C has just two unknown member forces. Assume both in tension.

sin γ = 4/6.403 = 0.6247, cos γ = 5/6.403 = 0.7809
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −3.333/0.6247 = −5.336 kN

Answer

FBC = −5.336 kN (compression)
6.Truss: method of joints

Answer: member BF

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 B

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

ΣF⊥ = 0 → FBF = 0

Check with the method of joints

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

AB: 36.25 kN (T), BC: 36.25 kN (T), CD: 23.75 kN (T), DE: 23.75 kN (T), FG: 37.5 kN (C), GH: 37.5 kN (C), AF: 1.768 kN (C), HE: 33.59 kN (C), BF: 0, CG: 15 kN (C), DH: 10 kN (T), FC: 1.768 kN (T), HC: 19.45 kN (T)

Answer

Zero-force member: BF
7.Frames & machines

Answer: FBC = 7.486 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 = √(2.4² + 2.5²) = 3.466 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·(2.5/3.466)·6 = 12·2.7
FBC = 7.486 kN (compression)

Answer

FBC = 7.486 kN
8.Frames & machines

Answer: A = 11.69 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.

Cable tension

T = (8 + 1.5/2)/0.6 = 14.58 kN

Components at A

Ax = T·cos β = 11.67 kN
Ay = 8 + 1.5 − T·sin β = 0.75 kN

Magnitude

A = √(11.67² + 0.75²) = 11.69 kN

Answer

A = 11.69 kN
9.Shear force & bending moment

Answer: C (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 = 57.33 kN, R2 = 40.67 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 = 106.7, MC = 197.3 kN·m, MD = 172, ME = 130.7, MF = 73.33, MG = 0

Answer

Mark C: MC = 197.3 kN·m
10.Shear force & bending moment

Answer: Mmax = 68.06 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. Maximum moment: since dM/dx = V, the bending moment has its peak where the shear force passes through zero, either at a point load or inside a distributed load.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 16·5 = 80 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·6 = 16·5·2.5
RB = 200/6 = 33.33 kN
ΣFy = 0: RA = 80 − 33.33 = 46.67 kN

Zero shear

The shear force starts at RA, stays constant over any unloaded part and falls with slope w inside the load.

RA − w·(x0 − 0) = 0
x0 = 0 + 46.67/16 = 2.917 m

Maximum moment

Mmax = RA·x0 − w·(x0 − 0)²/2 = 46.67·2.917 − 16·2.917²/2 = 68.06 kN·m

Answer

Mmax = 68.06 kN·m
11.Centroid & second moment of area

Answer: Ix = 8.619 × 10⁶ mm⁴

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 rectangles

Take the base at full width and the two legs above it (height h − t), so nothing is counted twice.

base: A1 = 180·16 = 2880 mm², y1 = 8 mm
two legs: A2 = 2·16·104 = 3328 mm², y2 = 16 + 104/2 = 68 mm

Centroid

ȳ = (2880·8 + 3328·68)/6208 = 40.16 mm

Parallel-axis theorem

base: 180·16³/12 + 2880·(8 − 40.16)² = 3.041 × 10⁶ mm⁴
two legs: 2·16·104³/12 + 3328·(68 − 40.16)² = 5.578 × 10⁶ mm⁴
Ix = 3.041 × 10⁶ + 5.578 × 10⁶
Ix = 8.619 × 10⁶ mm⁴ = 8.619 × 10⁶ mm⁴

Answer

Ix = 8.619 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 38.23 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 = 260·30 = 7800 mm², yf = 260 + 30/2 = 275 mm
web: Aw = 20·260 = 5200 mm², yw = 260/2 = 130 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (7800·275 + 5200·130)/13000 = 217 mm

Parallel-axis theorem

flange: 260·30³/12 + 7800·(275 − 217)² = 2.682 × 10⁷ mm⁴
web: 20·260³/12 + 5200·(130 − 217)² = 6.865 × 10⁷ mm⁴
Ix = 2.682 × 10⁷ + 6.865 × 10⁷ = 9.548 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 290 − 217 = 73 mm
σ = M·y/I = 5 × 10⁷·73/9.548 × 10⁷ = 38.23 MPa

Answer

σtop = 38.23 MPa

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