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 = (−15, 10, 20) N acts on an object while it moves in a straight line from point A(−1, 4, 2) to point B(−3, 2, −3). Coordinates are in metres. Find the work W done by the force.

F = (−15, 10, 20) NA(−1, 4, 2) mB(−3, 2, −3) m
W = J
2.Vectors: dot & cross productHard
xyzab

The unit vector n̂ is perpendicular to both a = (1, −2, −5) and b = (0, −3, −1) and has a positive z-component. Find its y-component n̂y.

a = (1, −2, −5)b = (0, −3, −1)n̂z > 0
n̂y =
3.Beam support reactionsMedium
P1​ = 20 kNP2​ = 60 kNABRA​RB​ = ?1.5 m2 m1.5 m

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

L = 5 mP1 = 20 kN at 1.5 mP2 = 60 kN at 3.5 m
RB = kN
4.Beam support reactionsHard
P = 30 kN, 45°Q = 20 kNABα = ?1.5 m2.5 m2 m

The simply supported beam has a pin at A and a roller at B. A load P acts at 1.5 m from A, inclined at 45° to the horizontal, and a vertical load Q acts at 4 m from A. Find the angle α between the total reaction force at the pin A and the horizontal.

L = 6 mP = 30 kN at 1.5 m, θ = 45°Q = 20 kN at 4 m
α = °
5.Truss: method of jointsMedium
ABBCACACB35 kN6 m1 m3 m

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

span = 6 mheight = 3 mB is 1 m from Avertical load = 35 kN
FAB = kN
6.Truss: method of jointsHard
ABBCACACB40 kN10 kN6 m2 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 2 m from Avertical load = 40 kNhorizontal load = 10 kN →
FBC = kN
7.Frames & machinesMedium
OAB300 NQ240 mm60 mmFO​ = ?

The bell crank shown turns about the pin O. A vertical force of 300 N at A (240 mm from O) is balanced by a horizontal force at B (60 mm above O). Find the magnitude of the pin reaction FO.

F = 300 NOA = 240 mmOB = 60 mm
FO = N
8.Frames & machinesHard
w = 5 kN/m4 kN1 m1.5 m1.5 mABCD

The beam AB of the wall bracket shown is pinned at A and propped by the strut CD (C is 1.5 m below A). The beam carries a uniform load of 5 kN/m over its full length and a point load of 4 kN at its free end B. Find the force FCD in the strut.

w = 5 kN/mP = 4 kNAD = 1 mAB = 2.5 mAC = 1.5 m
FCD = kN
9.Shear force & bending momentMedium
55 kN55 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.

55 kN @ 10 m55 kN @ 6 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
55 kN20 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.

55 kN @ 12 m20 kN @ 4 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)
11.Centroid & second moment of areaMedium
240140t = 8xdimensions in mm

A channel section lies with its open side up: a base plate 240 mm wide with two upright legs, 140 mm high overall. Base and legs are all 8 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.

b = 240 mmh = 140 mmt = 8 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
130230122401212xdimensions in mm

A welded I-section has a top flange 130 × 12 mm, a web 240 mm high and 12 mm thick, and a bottom flange 230 × 12 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 130 × 12 mmweb: 12 × 240 mmbottom flange: 230 × 12 mm
Ix = × 10⁶ mm⁴

3Solutions

1.Vectors: dot & cross product

Answer: W = −90 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 = (−3, 2, −3) − (−1, 4, 2) = (−2, −2, −5) m

Work

W = F·d = (−15)·(−2) + 10·(−2) + 20·(−5) = −90 J

Answer

W = −90 J

Negative work: the force acts mostly against the motion.

2.Vectors: dot & cross product

Answer: n̂y = −0.07474

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 = (−2)·(−1) − (−5)·(−3) = −13
(a × b)y = azbx − axbz = (−5)·0 − 1·(−1) = 1
(a × b)z = axby − aybx = 1·(−3) − (−2)·0 = −3

Normalise

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

|a × b| = √((−13)² + 1² + (−3)²) = 13.38
n̂ = −(−13, 1, −3)/13.38 = (0.9717, −0.07474, 0.2242)
n̂y = −0.07474

Answer

n̂y = −0.07474
3.Beam support reactions

Answer: RB = 48 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​ = 60 kNABRA​RB​1.5 m2 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·5 = 20·1.5 + 60·3.5
RB = 240/5 = 48 kN
ΣFy = 0: RA = 80 − 48 = 32 kN

Answer

RB = 48 kN
4.Beam support reactions

Answer: α = 46.78 °

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.

Components of P

Pv = 30·sin 45° = 21.21 kN
Ph = 30·cos 45° = 21.21 kN

Reactions

ΣMA = 0: RB·6 = 21.21·1.5 + 20·4 → RB = 18.64 kN
Ay = 21.21 + 20 − 18.64 = 22.58 kN
Ax = Ph = 21.21 kN

Direction at A

α = atan(Ay/Ax) = atan(22.58/21.21) = 46.78°

Answer

α = 46.78°
5.Truss: method of joints

Answer: FAB = −30.74 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.

ABBCACACB35 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 35·1 → Cy = 5.833 kN
ΣFy = 0: Ay = 35 − 5.833 = 29.17 kN

Joint A

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

sin α = 3/3.162 = 0.9487
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −29.17/0.9487 = −30.74 kN

Answer

FAB = −30.74 kN (compression)
6.Truss: method of joints

Answer: FBC = −28.28 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.

ABBCACACB40 kN10 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 40·2 + 10·4 → Cy = 20 kN
ΣFy = 0: Ay = 40 − 20 = 20 kN
ΣFx = 0: Ax = −10 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 = 4/5.657 = 0.7071, cos γ = 4/5.657 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −20/0.7071 = −28.28 kN

Answer

FBC = −28.28 kN (compression)
7.Frames & machines

Answer: FO = 1237 N

Machines: pliers, levers, linkages and clamps turn an input force into a larger or a differently directed output force. Draw one part as a free body and take moments about its pivot: the pin force drops out, and Fin·a = Fout·b gives the mechanical advantage a/b. The pin force then follows from ΣF = 0 on the same part. In a toggle, two links meet at a shallow angle θ; each link is a two-force member, so a small force F at the joint creates large link forces F/(2 sin θ) and a clamping force F/(2 tan θ).

Force at B

Q = 300·240/60 = 1200 N

Pin reaction

Ox = 1200 N, Oy = 300 N
FO = √(1200² + 300²) = 1237 N

Answer

FO = 1237 N
8.Frames & machines

Answer: FCD = 30.8 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.

Resultant of the uniform load

w·L = 5·2.5 = 12.5 kN at 1.25 m

Moments about A for the beam

FCD·0.8321·1 = 12.5·1.25 + 4·2.5 = 25.63 kN·m
FCD = 30.8 kN

Answer

FCD = 30.8 kN
9.Shear force & bending moment

Answer: D (x = 6 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 = 36.67 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 = 73.33, MC = 146.7, MD = 220 kN·m, ME = 183.3, MF = 146.7, MG = 0

Answer

Mark D: MD = 220 kN·m
10.Shear force & bending moment

Answer: F (x = 10 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 = 1 kN, R2 = 74 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 = 2, MC = 4, MD = −34, ME = −72, MF = −110 kN·m, MG = 0

Answer

Mark F: MF = −110 kN·m
11.Centroid & second moment of area

Answer: Ix = 8.005 × 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 = 240·8 = 1920 mm², y1 = 4 mm
two legs: A2 = 2·8·132 = 2112 mm², y2 = 8 + 132/2 = 74 mm

Centroid

ȳ = (1920·4 + 2112·74)/4032 = 40.67 mm

Parallel-axis theorem

base: 240·8³/12 + 1920·(4 − 40.67)² = 2.592 × 10⁶ mm⁴
two legs: 2·8·132³/12 + 2112·(74 − 40.67)² = 5.413 × 10⁶ mm⁴
Ix = 2.592 × 10⁶ + 5.413 × 10⁶
Ix = 8.005 × 10⁶ mm⁴ = 8.005 × 10⁶ mm⁴

Answer

Ix = 8.005 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 79.28 × 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 three rectangles

Measure every y from the bottom edge.

top flange: A = 1560 mm², y = 258 mm
web: A = 2880 mm², y = 132 mm
bottom flange: A = 2760 mm², y = 6 mm

Centroid

ȳ = (1560·258 + 2880·132 + 2760·6)/7200 = 111 mm

Parallel-axis theorem

top flange: 130·12³/12 + 1560·147² = 3.373 × 10⁷ mm⁴
web: 12·240³/12 + 2880·21² = 1.509 × 10⁷ mm⁴
bottom flange: 230·12³/12 + 2760·105² = 3.046 × 10⁷ mm⁴
Ix = 3.373 × 10⁷ + 1.509 × 10⁷ + 3.046 × 10⁷
Ix = 7.928 × 10⁷ mm⁴ = 79.28 × 10⁶ mm⁴

Answer

Ix = 79.28 × 10⁶ mm⁴

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