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 dot product a·b of a = (3, −7, −5) and b = (1, 3, −4).

a = (3, −7, −5)b = (1, 3, −4)
a·b =
2.Vectors: dot & cross productHard
xyzrFOA

A force F = (−40, 0, −30) N acts at point A(−2, −1, 1). Coordinates are in metres. Find the y-component My of the moment of the force about point O(1, −3, 2).

F = (−40, 0, −30) NA(−2, −1, 1) mO(1, −3, 2) m
My = N·m
3.Beam support reactionsMedium
w0​ = 20 kN/mP = 70 kNABRB​ = ?0.5 m5.5 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that falls from 20 kN/m at A to zero at B. A point load P also acts at 0.5 m from A. Find the vertical support reaction RB.

L = 6 mw0 = 20 kN/mP = 70 kN at 0.5 m
RB = kN
4.Beam support reactionsHard
w = 3 kN/mP = 15 kNABRA​RB​ = ?1 m2 m2 m

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

L = 5 mP = 15 kN at 1 mw = 3 kN/m from 3 to 5 m
RB = kN
5.Truss: method of jointsMedium
ABBCACACB55 kN6 m4 m4 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 = 4 mB is 4 m from Avertical load = 55 kN
FAB = kN
6.Truss: method of jointsHard
ABCDEFGH30 kN25 kN25 kN10 kN30 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.

D: 30 kN ↓F: 25 kN ↓F: 25 kN →G: 10 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
OAB300 NQ240 mm75 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 (75 mm above O). Find the magnitude of the pin reaction FO.

F = 300 NOA = 240 mmOB = 75 mm
FO = N
8.Frames & machinesHard
w = 3 kN/m10 kN1.6 m0.8 m0.5 mABCD

The beam AB of the wall bracket shown is pinned at A and propped by the strut CD (C is 0.5 m below A). The beam carries a uniform load of 3 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 = 3 kN/mP = 10 kNAD = 1.6 mAB = 2.4 mAC = 0.5 m
FCD = kN
9.Shear force & bending momentMedium
w = 8 kN/mABsection3 m7 m

Find the shear force Vx at the section x = 3 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mw = 8 kN/m from 0 to 10 mx = 3 m
Vx = kN
10.Shear force & bending momentHard
4 kN/m50 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.

50 kN @ 6 m4 kN/m, 0–5 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
1401530014xdimensions in mm

Find the second moment of area Ix of the T-section about the horizontal axis x through its centroid.

bf = 140 mmtf = 15 mmtw = 14 mmhw = 300 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
190160203901816xdimensions in mm

A welded I-section has a top flange 190 × 20 mm, a web 390 mm high and 16 mm thick, and a bottom flange 160 × 18 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 190 × 20 mmweb: 16 × 390 mmbottom flange: 160 × 18 mm
Ix = × 10⁶ mm⁴

3Solutions

1.Vectors: dot & cross product

Answer: a·b = 2

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.

Multiply matching components and add

a·b = 3·1 + (−7)·3 + (−5)·(−4) = 3 + (−21) + 20 = 2

Answer

a·b = 2

Positive: the angle between the vectors is less than 90°.

2.Vectors: dot & cross product

Answer: My = −50 N·m

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.

Position vector from O to A

r = A − O = (−2, −1, 1) − (1, −3, 2) = (−3, 2, −1) m

Moment M = r × F

(r × F)x = ryFz − rzFy = 2·(−30) − (−1)·0 = −60 N·m
(r × F)y = rzFx − rxFz = (−1)·(−40) − (−3)·(−30) = −50 N·m
(r × F)z = rxFy − ryFx = (−3)·0 − 2·(−40) = 80 N·m

Requested component

My = −50 N·m

Answer

My = −50 N·m
3.Beam support reactions

Answer: RB = 25.83 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 triangular load

W = ½·20·6 = 60 kN
x̄ = L/3 = 2 m

Equilibrium

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

ΣMA = 0: RB·6 = 60·2 + 70·0.5
RB = 25.83 kN
RA = 130 − 25.83 = 104.2 kN

Answer

RB = 25.83 kN
4.Beam support reactions

Answer: RB = 7.8 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 = 3 kN/mP = 15 kNABRA​RB​1 m2 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 = 3·2 = 6 kN, acting at x̄ = 4 m
ΣMA = 0: RB·5 = 15·1 + 3·2·4
RB = 39/5 = 7.8 kN
ΣFy = 0: RA = 21 − 7.8 = 13.2 kN

Answer

RB = 7.8 kN
5.Truss: method of joints

Answer: FAB = −25.93 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.

ABBCACACB55 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 55·4 → Cy = 36.67 kN
ΣFy = 0: Ay = 55 − 36.67 = 18.33 kN

Joint A

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

sin α = 4/5.657 = 0.7071
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −18.33/0.7071 = −25.93 kN

Answer

FAB = −25.93 kN (compression)
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: 70.42 kN (T), BC: 82.5 kN (T), CD: 82.5 kN (T), DE: 81.25 kN (T), FG: 70.42 kN (C), GH: 81.25 kN (C), AF: 56.77 kN (C), HE: 101.6 kN (C), BF: 9.063 kN (T), CG: 0, DH: 30.94 kN (T), BG: 15.1 kN (C), DG: 1.563 kN (C)

Answer

Zero-force member: CG
7.Frames & machines

Answer: FO = 1006 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 = 300·240/75 = 960 N

Pin reaction

Ox = 960 N, Oy = 300 N
FO = √(960² + 300²) = 1006 N

Answer

FO = 1006 N
8.Frames & machines

Answer: FCD = 68.39 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 = 3·2.4 = 7.2 kN at 1.2 m

Moments about A for the beam

FCD·0.2983·1.6 = 7.2·1.2 + 10·2.4 = 32.64 kN·m
FCD = 68.39 kN

Answer

FCD = 68.39 kN
9.Shear force & bending moment

Answer: Vx = 16 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 = 8·10 = 80 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 8·10·5
RB = 400/10 = 40 kN
ΣFy = 0: RA = 80 − 40 = 40 kN
w = 8 kN/mABRA​ = 40RB​ = 40section3 m7 m

Cut at x = 3 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 = 40 − 8·3 = 16 kN

Answer

Vx = 16 kN
10.Shear force & bending moment

Answer: F (x = 5 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 = 0 kN, R2 = 70 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 = −8, MD = −18, ME = −32, MF = −50 kN·m, MG = 0

Answer

Mark F: MF = −50 kN·m
11.Centroid & second moment of area

Answer: Ix = 66.27 × 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 two rectangles

Measure every y from the bottom edge.

flange: Af = 140·15 = 2100 mm², yf = 300 + 15/2 = 307.5 mm
web: Aw = 14·300 = 4200 mm², yw = 300/2 = 150 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2100·307.5 + 4200·150)/6300 = 202.5 mm

Parallel-axis theorem

flange: 140·15³/12 + 2100·(307.5 − 202.5)² = 2.319 × 10⁷ mm⁴
web: 14·300³/12 + 4200·(150 − 202.5)² = 4.308 × 10⁷ mm⁴
Ix = 2.319 × 10⁷ + 4.308 × 10⁷ = 6.627 × 10⁷ mm⁴ = 66.27 × 10⁶ mm⁴

Answer

Ix = 66.27 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 356 × 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 = 3800 mm², y = 418 mm
web: A = 6240 mm², y = 213 mm
bottom flange: A = 2880 mm², y = 9 mm

Centroid

ȳ = (3800·418 + 6240·213 + 2880·9)/12920 = 227.8 mm

Parallel-axis theorem

top flange: 190·20³/12 + 3800·190.2² = 1.376 × 10⁸ mm⁴
web: 16·390³/12 + 6240·14.82² = 8.046 × 10⁷ mm⁴
bottom flange: 160·18³/12 + 2880·218.8² = 1.38 × 10⁸ mm⁴
Ix = 1.376 × 10⁸ + 8.046 × 10⁷ + 1.38 × 10⁸
Ix = 3.56 × 10⁸ mm⁴ = 356 × 10⁶ mm⁴

Answer

Ix = 356 × 10⁶ mm⁴

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