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

F = (−25, 5, −10) NA(2, −4, −3) mB(3, −4, 1) m
W = J
2.Vectors: dot & cross productHard
xyzab

Find the area A of the parallelogram spanned by a = (−4, −5, 3) and b = (6, −2, 0).

a = (−4, −5, 3)b = (6, −2, 0)
A =
3.Beam support reactionsMedium
w = 5 kN/mP = 45 kNABRA​ = ?3 m3 m2 m

The cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w from the wall to 6 m and a point load P at 3 m from the wall. Find the vertical reaction RA at the wall.

L = 8 mP = 45 kN at 3 mw = 5 kN/m from 0 to 6 m
RA = kN
4.Beam support reactionsHard
w = 4 kN/mP = 65 kNABCRA​ = ?1 m0.5 m2.5 m1 m

The beam has a pin at A and a roller at B, 4 m from A, and overhangs B to the free end C. It carries a point load P at 1 m from A and a uniformly distributed load w from 1.5 m to the free end at 5 m. Find the vertical reaction RA, taking upward as positive.

AB = 4 mAC = 5 mP = 65 kN at 1 mw = 4 kN/m from 1.5 to 5 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB50 kN6 m4 m3 m

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

span = 6 mheight = 3 mB is 4 m from Avertical load = 50 kN
FAC = kN
6.Truss: method of jointsHard
ABCDEFGH30 kN40 kN15 kN15 kN10 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 ↓D: 40 kN ↓F: 15 kN ↓H: 15 kN ↓H: 10 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.Frames & machinesMedium
4 kN6 m2 m1.6 mABCDE

The A-frame shown stands on a pin at A and a roller at B, 6 m apart. The legs meet at the pin C, 3.6 m high, and the horizontal tie DE is 2 m above the ground. A load of 4 kN acts at C. Find the magnitude of the force C that the pin C exerts on leg BC.

P = 4 kNAB = 6 mheight of C = 3.6 mheight of DE = 2 m
C = kN
8.Frames & machinesHard
F = ?1500 N5 mmABC

A toggle press has two equal links AB and BC, each 200 mm long between pins. The joint B sits 5 mm above the line AC. Which downward force F at B produces a horizontal pressing force of 1500 N at the slider C? Neglect friction and weights.

Q = 1500 NAB = BC = 200 mmh = 5 mm
F = N
9.Shear force & bending momentMedium
P1​ = 15 kNP2​ = 15 kNAB2.5 m1 m1.5 m

The simply supported beam carries two point loads. Find the maximum bending moment Mmax in the beam.

L = 5 mP1 = 15 kN at 2.5 mP2 = 15 kN at 3.5 m
Mmax = kN·m
10.Shear force & bending momentHard
w = 4 kN/mP = 65 kNAB4 m6 m

The simply supported beam carries a uniformly distributed load w over its whole span and a point load P. Find the maximum bending moment Mmax in the beam.

L = 10 mP = 65 kN at 4 mw = 4 kN/m from 0 to 10 m
Mmax = kN·m
11.Centroid & second moment of areaMedium
150 mm240 mm96 mmØ50xIx​ = ?

A 150 mm × 240 mm plate has a circular hole of diameter 50 mm on its vertical centre line, with its centre 96 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 150 mmh = 240 mmd = 50 mmhole centre: y = 96 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
180210143201410xdimensions in mm

A welded I-section has a top flange 180 × 14 mm, a web 320 mm high and 10 mm thick, and a bottom flange 210 × 14 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 180 × 14 mmweb: 10 × 320 mmbottom flange: 210 × 14 mm
Ix = × 10⁶ mm⁴

3Solutions

1.Vectors: dot & cross product

Answer: W = −65 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, 1) − (2, −4, −3) = (1, 0, 4) m

Work

W = F·d = (−25)·1 + 5·0 + (−10)·4 = −65 J

Answer

W = −65 J

Negative work: the force acts mostly against the motion.

2.Vectors: dot & cross product

Answer: A = 42.47

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 = (−5)·0 − 3·(−2) = 6
(a × b)y = azbx − axbz = 3·6 − (−4)·0 = 18
(a × b)z = axby − aybx = (−4)·(−2) − (−5)·6 = 38

Area

A = |a × b| = √(6² + 18² + 38²) = 42.47

Answer

A = 42.47
3.Beam support reactions

Answer: RA = 75 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 = 5·6 = 30 kN, x̄ = 3 m

Vertical equilibrium

RA = P + W = 45 + 30 = 75 kN

Answer

RA = 75 kN
4.Beam support reactions

Answer: RA = 51.38 kN

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.

Resultant of the distributed load

W = 4·3.5 = 14 kN, x̄ = (1.5 + 5)/2 = 3.25 m

Equilibrium

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

ΣMA = 0: RB·4 = 65·1 + 14·3.25
RB = 110.5/4 = 27.63 kN
RA = 79 − 27.63 = 51.38 kN

Answer

RA = 51.38 kN
5.Truss: method of joints

Answer: FAC = 22.22 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.

ABBCACACB50 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 50·4 → Cy = 33.33 kN
ΣFy = 0: Ay = 50 − 33.33 = 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 = 3/3.606 = 0.8321, cos γ = 2/3.606 = 0.5547
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −33.33/0.8321 = −40.06 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−40.06)·0.5547 = 22.22 kN

Answer

FAC = 22.22 kN (tension)
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: 55.83 kN (T), BC: 61.67 kN (T), CD: 61.67 kN (T), DE: 67.5 kN (T), FG: 65.83 kN (C), GH: 77.5 kN (C), AF: 82.29 kN (C), HE: 84.37 kN (C), BF: 34.38 kN (T), CG: 0, DH: 35.63 kN (T), BG: 7.292 kN (C), DG: 7.292 kN (T)

Answer

Zero-force member: CG
7.Frames & machines

Answer: C = 4.25 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.

Tie force from leg BC

By = 2 kN
T = 2·3/1.6 = 3.75 kN

Components of the pin force on BC

Cx = T = 3.75 kN, Cy = −By = −2 kN

Magnitude

C = √(3.75² + 2²) = 4.25 kN

Answer

C = 4.25 kN
8.Frames & machines

Answer: F = 75.02 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).

Link angle

sin θ = 5/200 = 0.025, θ = 1.433°

Link force

Flink = Q/cos θ = 1500 N

Force at B

F = 2·Flink·sin θ = 2·1500·tan θ = 75.02 N

Answer

F = 75.02 N
9.Shear force & bending moment

Answer: Mmax = 30 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.

ΣMA = 0: RB·5 = 15·2.5 + 15·3.5
RB = 90/5 = 18 kN
ΣFy = 0: RA = 30 − 18 = 12 kN

Moment under each load

Keep the part left of each load.

under P1: M = RA·2.5 = 12·2.5 = 30 kN·m
under P2: M = RB·1.5 = 18·1.5 = 27 kN·m

Largest value

Mmax = 30 kN·m (under P1)

Answer

Mmax = 30 kN·m
10.Shear force & bending moment

Answer: Mmax = 204 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 = 4·10 = 40 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 65·4 + 4·10·5
RB = 460/10 = 46 kN
ΣFy = 0: RA = 105 − 46 = 59 kN

Where is V = 0?

V(4⁻) = RA − w·4 = 43 kN
V(4⁺) = 43 − 65 = −22 kN
The shear changes sign at the load, so the maximum is under the load.

Maximum moment

Mmax = RA·4 − w·4²/2 = 59·4 − 4·4²/2 = 204 kN·m

Answer

Mmax = 204 kN·m

It occurs at x = 4 m from A.

11.Centroid & second moment of area

Answer: Ix = 171.3 × 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 = (36000·120 − 1963·96)/(36000 − 1963) = 121.4 mm

Full plate about ȳ

150·240³/12 + 36000·−1.385² = 172.9 × 10⁶ mm⁴

Hole about ȳ

π·50⁴/64 + 1963·−25.38² = 1.572 × 10⁶ mm⁴

Subtract

Ix = 171.3 × 10⁶ mm⁴

Answer

Ix = 171.3 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 179.1 × 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 = 2520 mm², y = 341 mm
web: A = 3200 mm², y = 174 mm
bottom flange: A = 2940 mm², y = 7 mm

Centroid

ȳ = (2520·341 + 3200·174 + 2940·7)/8660 = 165.9 mm

Parallel-axis theorem

top flange: 180·14³/12 + 2520·175.1² = 7.73 × 10⁷ mm⁴
web: 10·320³/12 + 3200·8.099² = 2.752 × 10⁷ mm⁴
bottom flange: 210·14³/12 + 2940·158.9² = 7.428 × 10⁷ mm⁴
Ix = 7.73 × 10⁷ + 2.752 × 10⁷ + 7.428 × 10⁷
Ix = 1.791 × 10⁸ mm⁴ = 179.1 × 10⁶ mm⁴

Answer

Ix = 179.1 × 10⁶ mm⁴

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