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 angle θ between the vectors a = (1, 0, −1) and b = (6, −3, −1), in degrees.

a = (1, 0, −1)b = (6, −3, −1)
θ = °
2.Vectors: dot & cross productHard
xyzabc

Find the volume V of the parallelepiped whose edges from one corner are a = (3, 5, 4), b = (−3, 4, 3) and c = (−3, 5, 3).

a = (3, 5, 4)b = (−3, 4, 3)c = (−3, 5, 3)
V =
3.Beam support reactionsMedium
P1​ = 15 kNP2​ = 60 kNABRA​RB​ = ?3 m2 m5 m

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

L = 10 mP1 = 15 kN at 3 mP2 = 60 kN at 5 m
RB = kN
4.Beam support reactionsHard
w = 10 kN/mP = 60 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 RB.

L = 4 mP = 60 kN at 2 mw = 10 kN/m from 0 to 1 m
RB = kN
5.Truss: method of jointsMedium
ABBCACACB30 kN6 m2 m2 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 = 2 mB is 2 m from Avertical load = 30 kN
FAC = kN
6.Truss: method of jointsHard
ABCDEFGH40 kN25 kN10 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.

B: 40 kN ↓H: 25 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
8 kN1.6 m2.4 m1.5 mABCD

A horizontal beam AB is pinned to a wall at A and propped by the strut CD, pinned to the wall at C, 1.5 m below A. A load of 8 kN hangs at B. Neglect the weights. Find the magnitude of the pin force A on the beam at A.

P = 8 kNAD = 1.6 mAB = 4 mAC = 1.5 m
A = kN
8.Frames & machinesHard
w = 1 kN/m10 kN1.6 m0.9 m1.2 mABCD

The beam AB of the wall bracket shown is pinned at A and propped by the strut CD (C is 1.2 m below A). The beam carries a uniform load of 1 kN/m over its full length and a point load of 10 kN at its free end B. Find the force FCD in the strut.

w = 1 kN/mP = 10 kNAD = 1.6 mAB = 2.5 mAC = 1.2 m
FCD = kN
9.Shear force & bending momentMedium
w = 5 kN/mABsection1.5 m2.5 m

Find the shear force Vx at the section x = 1.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mw = 5 kN/m from 0 to 4 mx = 1.5 m
Vx = kN
10.Shear force & bending momentHard
25 kN50 kN50 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 m50 kN @ 6 m50 kN @ 2 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
120 mm240 mm84 mmØ50xIx​ = ?

A 120 mm × 240 mm plate has a circular hole of diameter 50 mm on its vertical centre line, with its centre 84 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 120 mmh = 240 mmd = 50 mmhole centre: y = 84 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
120 mm300 mm105 mm50 × 50xIx​ = ?

A 120 mm × 300 mm plate has a rectangular cut-out 50 mm wide and 50 mm high, centred on the vertical centre line with its centre 105 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 120 mmh = 300 mmcut-out: 50 × 50 mmhole centre: y = 105 mm
Ix = × 10⁶ mm⁴

3Solutions

1.Vectors: dot & cross product

Answer: θ = 43.13 °

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.

Dot product

a·b = 1·6 + 0·(−3) + (−1)·(−1) = 7

Magnitudes

|a| = √(1² + 0² + (−1)²) = 1.414
|b| = √(6² + (−3)² + (−1)²) = 6.782

Angle

cos θ = 7/(1.414·6.782) = 0.7298
θ = arccos(0.7298) = 43.13°

Answer

θ = 43.13°
2.Vectors: dot & cross product

Answer: V = 21

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 b × c

(b × c)x = bycz − bzcy = 4·3 − 3·5 = −3
(b × c)y = bzcx − bxcz = 3·(−3) − (−3)·3 = 0
(b × c)z = bxcy − bycx = (−3)·5 − 4·(−3) = −3

Dot product with a

a·(b × c) = 3·(−3) + 5·0 + 4·(−3) = −21
V = |−21| = 21

Answer

V = 21
3.Beam support reactions

Answer: RB = 34.5 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.

P1​ = 15 kNP2​ = 60 kNABRA​RB​3 m2 m5 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 = 15·3 + 60·5
RB = 345/10 = 34.5 kN
ΣFy = 0: RA = 75 − 34.5 = 40.5 kN

Answer

RB = 34.5 kN
4.Beam support reactions

Answer: RB = 31.25 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 = 10 kN/mP = 60 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 = 10·1 = 10 kN, acting at x̄ = 0.5 m
ΣMA = 0: RB·4 = 60·2 + 10·1·0.5
RB = 125/4 = 31.25 kN
ΣFy = 0: RA = 70 − 31.25 = 38.75 kN

Answer

RB = 31.25 kN
5.Truss: method of joints

Answer: FAC = 20 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.

ABBCACACB30 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 30·2 → Cy = 10 kN
ΣFy = 0: Ay = 30 − 10 = 20 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 = 2/4.472 = 0.4472, cos γ = 4/4.472 = 0.8944
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −10/0.4472 = −22.36 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−22.36)·0.8944 = 20 kN

Answer

FAC = 20 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: 28.75 kN (T), BC: 27.5 kN (T), CD: 27.5 kN (T), DE: 26.25 kN (T), FG: 38.75 kN (C), GH: 36.25 kN (C), AF: 54.8 kN (C), HE: 37.12 kN (C), BF: 38.75 kN (T), CG: 0, DH: 1.25 kN (T), BG: 1.768 kN (T), DG: 1.768 kN (C)

Answer

Zero-force member: CG
7.Frames & machines

Answer: A = 24.48 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.

Strut force

FCD = 8·4/(0.6839·1.6) = 29.24 kN

Components at A

Ax = FCD·cos α = 21.33 kN (towards the wall)
Ay = 8 − FCD·sin α = −12 kN

Magnitude

A = √(21.33² + −12²) = 24.48 kN

Answer

A = 24.48 kN

A negative Ay means the wall pulls the beam down at A.

8.Frames & machines

Answer: FCD = 29.3 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 = 1·2.5 = 2.5 kN at 1.25 m

Moments about A for the beam

FCD·0.6·1.6 = 2.5·1.25 + 10·2.5 = 28.13 kN·m
FCD = 29.3 kN

Answer

FCD = 29.3 kN
9.Shear force & bending moment

Answer: Vx = 2.5 kN

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 = 5·4 = 20 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 5·4·2
RB = 40/4 = 10 kN
ΣFy = 0: RA = 20 − 10 = 10 kN
w = 5 kN/mABRA​ = 10RB​ = 10section1.5 m2.5 m

Cut at x = 1.5 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.

V = RA − (all downward loads left of the cut)
Vx = 10 − 5·1.5 = 2.5 kN

Answer

Vx = 2.5 kN
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 = 33.33 kN, R2 = 91.67 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 = −25, MC = −16.67, MD = −58.33, ME = −100 kN·m, MF = −50, MG = 0

Answer

Mark E: ME = −100 kN·m
11.Centroid & second moment of area

Answer: Ix = 135.2 × 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 = (28800·120 − 1963·84)/(28800 − 1963) = 122.6 mm

Full plate about ȳ

120·240³/12 + 28800·−2.634² = 138.4 × 10⁶ mm⁴

Hole about ȳ

π·50⁴/64 + 1963·−38.63² = 3.237 × 10⁶ mm⁴

Subtract

Ix = 135.2 × 10⁶ mm⁴

Answer

Ix = 135.2 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 264 × 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 = (36000·150 − 2500·105)/(36000 − 2500) = 153.4 mm

Full plate about ȳ

120·300³/12 + 36000·−3.358² = 270.4 × 10⁶ mm⁴

Hole about ȳ

50·50³/12 + 2500·−48.36² = 6.367 × 10⁶ mm⁴

Subtract

Ix = 264 × 10⁶ mm⁴

Answer

Ix = 264 × 10⁶ mm⁴

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