Statics: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

New problemsBack to the course

In the print window, choose “Save as PDF” to keep a copy on your device.

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, −6, 3) and b = (0, −1, 3), in degrees.

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

Find the volume V of the parallelepiped whose edges from one corner are a = (−2, 0, −5), b = (−2, 5, 2) and c = (−3, 0, 4).

a = (−2, 0, −5)b = (−2, 5, 2)c = (−3, 0, 4)
V =
3.Beam support reactionsMedium
P1​ = 10 kNP2​ = 50 kNABRA​RB​ = ?2 m0.5 m1.5 m

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

L = 4 mP1 = 10 kN at 2 mP2 = 50 kN at 2.5 m
RB = kN
4.Beam support reactionsHard
w = 5 kN/mP = 60 kNABRA​RB​ = ?1 m1 m1 m1 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 = 5 kN/m from 1 to 3 m
RB = kN
5.Truss: method of jointsMedium
ABCDEFGH30 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.

F: 30 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
ABCDEFGH15 kN35 kN30 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: 15 kN ↓F: 35 kN →H: 30 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
12 kN1.6 m0.8 m0.75 mABCD

A horizontal beam AB is pinned to a wall at A and propped by the strut CD, pinned to the wall at C, 0.75 m below A. A load of 12 kN hangs at B. Neglect the weights. Find the magnitude of the pin force A on the beam at A.

P = 12 kNAD = 1.6 mAB = 2.4 mAC = 0.75 m
A = kN
8.Frames & machinesHard
15 kN3 kN2 m2.5 mABC

A uniform horizontal boom AB of weight 3 kN is pinned to a wall at A and held by a cable from its end B to the point C on the wall, 2.5 m above A. A load of 15 kN hangs at B. Find the tension T in the cable.

W = 15 kNWb = 3 kNAB = 2 mAC = 2.5 m
T = kN
9.Shear force & bending momentMedium
w = 5 kN/mABsection0.5 m9.5 m

Find the bending moment Mx at the section x = 0.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mw = 5 kN/m from 0 to 10 mx = 0.5 m
Mx = kN·m
10.Shear force & bending momentHard
w = 4 kN/mP = 40 kNAB2.5 m1.5 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 = 4 mP = 40 kN at 2.5 mw = 4 kN/m from 0 to 4 m
Mmax = kN·m
11.Centroid & second moment of areaMedium
1405001812xdimensions in mm

A symmetric I-section has flanges 140 mm wide and 18 mm thick, an overall depth of 500 mm and a web 12 mm thick. Find its elastic section modulus Sx for bending about the horizontal centroidal axis x.

B = 140 mmH = 500 mmtf = 18 mmtw = 12 mm
Sx = × 10³ mm³
12.Centroid & second moment of areaHard
19026018190188xdimensions in mm

A welded I-section has a top flange 190 × 18 mm, a web 190 mm high and 8 mm thick, and a bottom flange 260 × 18 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 190 × 18 mmweb: 8 × 190 mmbottom flange: 260 × 18 mm
Ix = × 10⁶ mm⁴

3Solutions

1.Vectors: dot & cross product

Answer: θ = 45.62 °

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 = 1·0 + (−6)·(−1) + 3·3 = 15

Magnitudes

|a| = √(1² + (−6)² + 3²) = 6.782
|b| = √(0² + (−1)² + 3²) = 3.162

Angle

cos θ = 15/(6.782·3.162) = 0.6994
θ = arccos(0.6994) = 45.62°

Answer

θ = 45.62°
2.Vectors: dot & cross product

Answer: V = 115

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 = 5·4 − 2·0 = 20
(b × c)y = bzcx − bxcz = 2·(−3) − (−2)·4 = 2
(b × c)z = bxcy − bycx = (−2)·0 − 5·(−3) = 15

Dot product with a

a·(b × c) = (−2)·20 + 0·2 + (−5)·15 = −115
V = |−115| = 115

Answer

V = 115
3.Beam support reactions

Answer: RB = 36.25 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.

P1​ = 10 kNP2​ = 50 kNABRA​RB​2 m0.5 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·4 = 10·2 + 50·2.5
RB = 145/4 = 36.25 kN
ΣFy = 0: RA = 60 − 36.25 = 23.75 kN

Answer

RB = 36.25 kN
4.Beam support reactions

Answer: RB = 35 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 = 5 kN/mP = 60 kNABRA​RB​1 m1 m1 m1 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 = 5·2 = 10 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 60·2 + 5·2·2
RB = 140/4 = 35 kN
ΣFy = 0: RA = 70 − 35 = 35 kN

Answer

RB = 35 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: 22.5 kN (T), BC: 15 kN (T), CD: 15 kN (T), DE: 7.5 kN (T), FG: 22.5 kN (C), GH: 7.5 kN (C), AF: 31.82 kN (C), HE: 10.61 kN (C), BF: 7.5 kN (C), CG: 0, DH: 7.5 kN (T), BG: 10.61 kN (T), DG: 10.61 kN (C)

Answer

Zero-force member: CG
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: 37.5 kN (T), BC: 40 kN (T), CD: 40 kN (T), DE: 42.5 kN (T), FG: 37.5 kN (C), GH: 42.5 kN (C), AF: 3.536 kN (C), HE: 60.1 kN (C), BF: 2.5 kN (T), CG: 0, DH: 12.5 kN (T), BG: 3.536 kN (C), DG: 3.536 kN (T)

Answer

Zero-force member: CG
7.Frames & machines

Answer: A = 38.87 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 = 12·2.4/(0.4244·1.6) = 42.41 kN

Components at A

Ax = FCD·cos α = 38.4 kN (towards the wall)
Ay = 12 − FCD·sin α = −6 kN

Magnitude

A = √(38.4² + −6²) = 38.87 kN

Answer

A = 38.87 kN

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

8.Frames & machines

Answer: T = 21.13 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 angle

BC = √(2² + 2.5²) = 3.202 m, sin β = 0.7809

Moments about A

T·0.7809·2 = 15·2 + 3·1
T = 21.13 kN

Answer

T = 21.13 kN
9.Shear force & bending moment

Answer: Mx = 11.88 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 = 5·10 = 50 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 5·10·5
RB = 250/10 = 25 kN
ΣFy = 0: RA = 50 − 25 = 25 kN
w = 5 kN/mABRA​ = 25RB​ = 25section0.5 m9.5 m

Cut at x = 0.5 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.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 25·0.5 − 5·0.5·0.25 = 11.88 kN·m

Answer

Mx = 11.88 kN·m
10.Shear force & bending moment

Answer: Mmax = 45 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 = 4·4 = 16 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 40·2.5 + 4·4·2
RB = 132/4 = 33 kN
ΣFy = 0: RA = 56 − 33 = 23 kN

Where is V = 0?

V(2.5⁻) = RA − w·2.5 = 13 kN
V(2.5⁺) = 13 − 40 = −27 kN
The shear changes sign at the load, so the maximum is under the load.

Maximum moment

Mmax = RA·2.5 − w·2.5²/2 = 23·2.5 − 4·2.5²/2 = 45 kN·m

Answer

Mmax = 45 kN·m

It occurs at x = 2.5 m from A.

11.Centroid & second moment of area

Answer: Sx = 1571 × 10³ mm³

Second moment of area: for a rectangle about its own centroidal axis I = bh³/12, and about its base bh³/3 (parallel-axis theorem I = Ic + A·d²). A hole is handled by subtracting its I, as long as both parts share the same axis. The elastic section modulus is S = I/c, where c is the distance to the extreme fibre.

Outer rectangle minus the two side cut-outs

Both cut-outs together are (B − tw) wide and hw = H − 2tf high, and share the axis x.

hw = 500 − 2·18 = 464 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (140·500³ − 128·464³)/12
Ix = 3.928 × 10⁸ mm⁴

Section modulus

c = H/2 = 250 mm
Sx = I/c = 3.928 × 10⁸/250
Sx = 1.571 × 10⁶ mm³ = 1571 × 10³ mm³

Answer

Sx = 1571 × 10³ mm³
12.Centroid & second moment of area

Answer: Ix = 90.62 × 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 = 3420 mm², y = 217 mm
web: A = 1520 mm², y = 113 mm
bottom flange: A = 4680 mm², y = 9 mm

Centroid

ȳ = (3420·217 + 1520·113 + 4680·9)/9620 = 99.38 mm

Parallel-axis theorem

top flange: 190·18³/12 + 3420·117.6² = 4.741 × 10⁷ mm⁴
web: 8·190³/12 + 1520·13.62² = 4.855 × 10⁶ mm⁴
bottom flange: 260·18³/12 + 4680·90.38² = 3.835 × 10⁷ mm⁴
Ix = 4.741 × 10⁷ + 4.855 × 10⁶ + 3.835 × 10⁷
Ix = 9.062 × 10⁷ mm⁴ = 90.62 × 10⁶ mm⁴

Answer

Ix = 90.62 × 10⁶ mm⁴

ExamProblems · examproblems.com/courses/statics