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 = (10, −20, 20) N acts on an object while it moves in a straight line from point A(−3, −5, 5) to point B(3, 4, −5). Coordinates are in metres. Find the work W done by the force.

F = (10, −20, 20) NA(−3, −5, 5) mB(3, 4, −5) m
W = J
2.Vectors: dot & cross productHard
xyzABC

Find the area A of the triangle with corners A(4, 4, 4), B(0, 1, 3) and C(4, −2, 0). Coordinates are in metres.

A(4, 4, 4)B(0, 1, 3)C(4, −2, 0)
A = m²
3.Beam support reactionsMedium
w = 2 kN/mP = 50 kNABRA​ = ?2 m2 m

The cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w from the wall to 2 m and a point load P at 2 m from the wall. Find the vertical reaction RA at the wall.

L = 4 mP = 50 kN at 2 mw = 2 kN/m from 0 to 2 m
RA = kN
4.Beam support reactionsHard
w = 12 kN/mP = 40 kNABRA​ = ?RB​1 m1 m2 m

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

L = 4 mP = 40 kN at 2 mw = 12 kN/m from 0 to 1 m
RA = kN
5.Truss: method of jointsMedium
ABCDEFGH10 kN15 kN15 kN4 × 4 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.

D: 10 kN ↓F: 15 kN ↓H: 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 BG
  13. 13member DG
6.Truss: method of jointsHard
ABBCACACB35 kN25 kN8 m5 m3 m

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

span = 8 mheight = 3 mB is 5 m from Avertical load = 35 kNhorizontal load = 25 kN →
FBC = kN
7.Frames & machinesMedium
OAB200 NQ150 mm150 mmFO​ = ?

The bell crank shown turns about the pin O. A vertical force of 200 N at A (150 mm from O) is balanced by a horizontal force at B (150 mm above O). Find the magnitude of the pin reaction FO.

F = 200 NOA = 150 mmOB = 150 mm
FO = N
8.Frames & machinesHard
10 kN3 m1 m2 mABCDE

The A-frame shown stands on a pin at A and a roller at B, 3 m apart. The legs meet at the pin C, 3 m high, and are tied by the horizontal bar DE at 1 m. A horizontal force of 10 kN to the right acts at C. Find the tension T in the tie.

P = 10 kNAB = 3 mheight of C = 3 mheight of DE = 1 m
T = kN
9.Shear force & bending momentMedium
w = 12 kN/mABsection4 m4 m

Find the bending moment Mx at the section x = 4 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mw = 12 kN/m from 0 to 8 mx = 4 m
Mx = kN·m
10.Shear force & bending momentHard
12 kN/m50 kN50 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 @ 12 m50 kN @ 4 m12 kN/m, 0–8 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
100 mm300 mm195 mmØ50xIx​ = ?

A 100 mm × 300 mm plate has a circular hole of diameter 50 mm on its vertical centre line, with its centre 195 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 100 mmh = 300 mmd = 50 mmhole centre: y = 195 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
240151608xsagging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 60 MPa in tension and 150 MPa in compression. Find the largest sagging bending moment Mallow the beam can carry.

bf = 240 mmtf = 15 mmtw = 8 mmhw = 160 mmσt,allow = 60 MPaσc,allow = 150 MPa
Mallow = kN·m

3Solutions

1.Vectors: dot & cross product

Answer: W = −320 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, 4, −5) − (−3, −5, 5) = (6, 9, −10) m

Work

W = F·d = 10·6 + (−20)·9 + 20·(−10) = −320 J

Answer

W = −320 J

Negative work: the force acts mostly against the motion.

2.Vectors: dot & cross product

Answer: A = 14.73 m²

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.

Edge vectors

AB = B − A = (−4, −3, −1)
AC = C − A = (0, −6, −4)

Cross product

(AB × AC)x = AByACz − ABzACy = (−3)·(−4) − (−1)·(−6) = 6
(AB × AC)y = ABzACx − ABxACz = (−1)·0 − (−4)·(−4) = −16
(AB × AC)z = ABxACy − AByACx = (−4)·(−6) − (−3)·0 = 24
|AB × AC| = √(6² + (−16)² + 24²) = 29.46

Area of the triangle

A = ½·29.46 = 14.73 m²

Answer

A = 14.73 m²
3.Beam support reactions

Answer: RA = 54 kN

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 = 2·2 = 4 kN, x̄ = 1 m

Vertical equilibrium

RA = P + W = 50 + 4 = 54 kN

Answer

RA = 54 kN
4.Beam support reactions

Answer: RA = 30.5 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 = 40 kNABRA​RB​1 m1 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.

UDL resultant: W = w·ℓ = 12·1 = 12 kN, acting at x̄ = 0.5 m
ΣMA = 0: RB·4 = 40·2 + 12·1·0.5
RB = 86/4 = 21.5 kN
ΣFy = 0: RA = 52 − 21.5 = 30.5 kN

Answer

RA = 30.5 kN
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 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: 17.5 kN (T), BC: 20 kN (T), CD: 20 kN (T), DE: 22.5 kN (T), FG: 17.5 kN (C), GH: 22.5 kN (C), AF: 24.75 kN (C), HE: 31.82 kN (C), BF: 2.5 kN (T), CG: 0, DH: 7.5 kN (T), BG: 3.536 kN (C), DG: 3.536 kN (T)

Answer

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

Answer: FBC = −44.19 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 kN25 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 35·5 + 25·3 → Cy = 31.25 kN
ΣFy = 0: Ay = 35 − 31.25 = 3.75 kN
ΣFx = 0: Ax = −25 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 = 3/4.243 = 0.7071, cos γ = 3/4.243 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −31.25/0.7071 = −44.19 kN

Answer

FBC = −44.19 kN (compression)
7.Frames & machines

Answer: FO = 282.8 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 = 200·150/150 = 200 N

Pin reaction

Ox = 200 N, Oy = 200 N
FO = √(200² + 200²) = 282.8 N

Answer

FO = 282.8 N
8.Frames & machines

Answer: T = 7.5 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·3 = 10·3
By = 10 kN

Leg BC: moments about C

10·1.5 = T·2
T = 7.5 kN

Answer

T = 7.5 kN

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

9.Shear force & bending moment

Answer: Mx = 96 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 = 12·8 = 96 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 12·8·4
RB = 384/8 = 48 kN
ΣFy = 0: RA = 96 − 48 = 48 kN
w = 12 kN/mABRA​ = 48RB​ = 48section4 m4 m

Cut at x = 4 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 = 48·4 − 12·4·2 = 96 kN·m

Answer

Mx = 96 kN·m
10.Shear force & bending moment

Answer: E (x = 8 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 = 48 kN, R2 = 148 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 = 72, MC = 96, MD = −28, ME = −200 kN·m, MF = −100, MG = 0

Answer

Mark E: ME = −200 kN·m
11.Centroid & second moment of area

Answer: Ix = 220.4 × 10⁶ mm⁴

Sections with holes: treat a hole as a negative area. The centroid is ȳ = (A₁y₁ − A₂y₂)/(A₁ − A₂), with A₁, y₁ for the full plate and A₂, y₂ for the hole. For the second moment of area about the centroidal axis, use the parallel-axis theorem for each part and subtract the hole: I = (Ic1 + A₁d₁²) − (Ic2 + A₂d₂²), where d is the distance from each part's own centroid to the axis through ȳ. A rectangle has Ic = bh³/12 and a circle Ic = πd⁴/64.

Centroid

ȳ = (30000·150 − 1963·195)/(30000 − 1963) = 146.8 mm

Full plate about ȳ

100·300³/12 + 30000·3.152² = 225.3 × 10⁶ mm⁴

Hole about ȳ

π·50⁴/64 + 1963·48.15² = 4.859 × 10⁶ mm⁴

Subtract

Ix = 220.4 × 10⁶ mm⁴

Answer

Ix = 220.4 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 4.162 kN·m

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.

Centroid

ȳ = (3600·167.5 + 1280·80)/4880 = 144.5 mm
top edge: c = 175 − 144.5 = 30.45 mm

Second moment of area

I = 240·15³/12 + 3600·22.95² + 8·160³/12 + 1280·64.55² = 1.003 × 10⁷ mm⁴

Moment allowed by each edge

Sagging: the top is in compression, the bottom in tension.

top edge: M = 150·1.003 × 10⁷/30.45 = 49.4 kN·m
bottom edge: M = 60·1.003 × 10⁷/144.5 = 4.162 kN·m

Governing value

Mallow = min = 4.162 kN·m (bottom edge)

Answer

Mallow = 4.162 kN·m

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