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 = (4, 5, 6) and b = (−6, 6, 7).

a = (4, 5, 6)b = (−6, 6, 7)
a·b =
2.Vectors: dot & cross productHard
xyzab

Find the area A of the parallelogram spanned by a = (−1, −2, −3) and b = (−6, 6, −5).

a = (−1, −2, −3)b = (−6, 6, −5)
A =
3.Beam support reactionsMedium
w0​ = 8 kN/mP = 30 kNABRA​ = ?3.5 m1.5 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that falls from 8 kN/m at A to zero at B. A point load P also acts at 3.5 m from A. Find the vertical support reaction RA.

L = 5 mw0 = 8 kN/mP = 30 kN at 3.5 m
RA = kN
4.Beam support reactionsHard
w = 10 kN/mP = 40 kNABCRB​ = ?0.5 m2 m1.5 m

The beam has a pin at A and a roller at B, 2.5 m from A, and overhangs B to the free end C. It carries a point load P at 0.5 m from A and a uniformly distributed load w from 2.5 m to the free end at 4 m. Find the vertical reaction RB, taking upward as positive.

AB = 2.5 mAC = 4 mP = 40 kN at 0.5 mw = 10 kN/m from 2.5 to 4 m
RB = kN
5.Truss: method of jointsMedium
ABBCACACB45 kN6 m5 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 5 m from Avertical load = 45 kN
FAC = kN
6.Truss: method of jointsHard
ABCDEFGH25 kN20 kN30 kN35 kN20 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: 25 kN ↓F: 20 kN ↓G: 30 kN ↓H: 35 kN ↓H: 20 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
100 NQ = ?5°ABC

In the toggle clamp shown, two equal links AB and BC are pinned together at B, and each makes 5° with the line AC. A downward force of 100 N is applied at B. The slider C presses on a workpiece. Neglecting friction and weights, find the horizontal clamping force Q.

F = 100 Nθ = 5°
Q = N
8.Frames & machinesHard
15 kN3.2 m1 m2.6 mABCDE

The A-frame shown stands on a pin at A and a roller at B, 3.2 m apart. The legs meet at the pin C, 3.6 m high, and are tied by the horizontal bar DE at 1 m. A horizontal force of 15 kN to the right acts at C. Find the tension T in the tie.

P = 15 kNAB = 3.2 mheight of C = 3.6 mheight of DE = 1 m
T = kN
9.Shear force & bending momentMedium
4 kN/m40 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.

40 kN @ 4 m4 kN/m, 4–12 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)
10.Shear force & bending momentHard
w = 12 kN/mP = 30 kNAB4 m1 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 = 5 mP = 30 kN at 4 mw = 12 kN/m from 0 to 5 m
Mmax = kN·m
11.Centroid & second moment of areaMedium
2401512012xdimensions in mm

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

bf = 240 mmtf = 15 mmtw = 12 mmhw = 120 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
110160103301414xdimensions in mm

A welded I-section has a top flange 110 × 10 mm, a web 330 mm high and 14 mm thick, and a bottom flange 160 × 14 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 110 × 10 mmweb: 14 × 330 mmbottom flange: 160 × 14 mm
Ix = × 10⁶ mm⁴

3Solutions

1.Vectors: dot & cross product

Answer: a·b = 48

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 = 4·(−6) + 5·6 + 6·7 = (−24) + 30 + 42 = 48

Answer

a·b = 48

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

2.Vectors: dot & cross product

Answer: A = 35.74

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 = (−2)·(−5) − (−3)·6 = 28
(a × b)y = azbx − axbz = (−3)·(−6) − (−1)·(−5) = 13
(a × b)z = axby − aybx = (−1)·6 − (−2)·(−6) = −18

Area

A = |a × b| = √(28² + 13² + (−18)²) = 35.74

Answer

A = 35.74
3.Beam support reactions

Answer: RA = 22.33 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 = ½·8·5 = 20 kN
x̄ = L/3 = 1.667 m

Equilibrium

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

ΣMA = 0: RB·5 = 20·1.667 + 30·3.5
RB = 27.67 kN
RA = 50 − 27.67 = 22.33 kN

Answer

RA = 22.33 kN
4.Beam support reactions

Answer: RB = 27.5 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 = 10·1.5 = 15 kN, x̄ = (2.5 + 4)/2 = 3.25 m

Equilibrium

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

ΣMA = 0: RB·2.5 = 40·0.5 + 15·3.25
RB = 68.75/2.5 = 27.5 kN
RA = 55 − 27.5 = 27.5 kN

Answer

RB = 27.5 kN
5.Truss: method of joints

Answer: FAC = 18.75 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.

ABBCACACB45 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 45·5 → Cy = 37.5 kN
ΣFy = 0: Ay = 45 − 37.5 = 7.5 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 = 2/2.236 = 0.8944, cos γ = 1/2.236 = 0.4472
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −37.5/0.8944 = −41.93 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−41.93)·0.4472 = 18.75 kN

Answer

FAC = 18.75 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: 42.5 kN (T), BC: 60 kN (T), CD: 60 kN (T), DE: 47.5 kN (T), FG: 62.5 kN (C), GH: 67.5 kN (C), AF: 88.39 kN (C), HE: 67.18 kN (C), BF: 42.5 kN (T), CG: 0, DH: 12.5 kN (T), BG: 24.75 kN (C), DG: 17.68 kN (C)

Answer

Zero-force member: CG
7.Frames & machines

Answer: Q = 571.5 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).

Equilibrium of pin B

2·Flink·sin 5° = 100
Flink = 573.7 N

Clamping force

Q = Flink·cos 5° = 100/(2·tan 5°) = 571.5 N

Answer

Q = 571.5 N

The force ratio Q/F = 5.715 grows without limit as the links straighten.

8.Frames & machines

Answer: T = 10.38 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·3.2 = 15·3.6
By = 16.88 kN

Leg BC: moments about C

16.88·1.6 = T·2.6
T = 10.38 kN

Answer

T = 10.38 kN

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

9.Shear force & bending moment

Answer: C (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 = 37.33 kN, R2 = 34.67 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 = 74.67, MC = 149.3 kN·m, MD = 136, ME = 106.7, MF = 61.33, MG = 0

Answer

Mark C: MC = 149.3 kN·m
10.Shear force & bending moment

Answer: Mmax = 54 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 = 12·5 = 60 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 30·4 + 12·5·2.5
RB = 270/5 = 54 kN
ΣFy = 0: RA = 90 − 54 = 36 kN

Where is V = 0?

RA − w·x0 = 0 → x0 = 36/12 = 3 m

Maximum moment

Mmax = RA·x0 − w·x0²/2 = 36·3 − 12·3²/2 = 54 kN·m

Answer

Mmax = 54 kN·m

It occurs at x = 3 m from A.

11.Centroid & second moment of area

Answer: Ix = 6.482 × 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 = 240·15 = 3600 mm², yf = 120 + 15/2 = 127.5 mm
web: Aw = 12·120 = 1440 mm², yw = 120/2 = 60 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3600·127.5 + 1440·60)/5040 = 108.2 mm

Parallel-axis theorem

flange: 240·15³/12 + 3600·(127.5 − 108.2)² = 1.406 × 10⁶ mm⁴
web: 12·120³/12 + 1440·(60 − 108.2)² = 5.075 × 10⁶ mm⁴
Ix = 1.406 × 10⁶ + 5.075 × 10⁶ = 6.482 × 10⁶ mm⁴ = 6.482 × 10⁶ mm⁴

Answer

Ix = 6.482 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 135.1 × 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 = 1100 mm², y = 349 mm
web: A = 4620 mm², y = 179 mm
bottom flange: A = 2240 mm², y = 7 mm

Centroid

ȳ = (1100·349 + 4620·179 + 2240·7)/7960 = 154.1 mm

Parallel-axis theorem

top flange: 110·10³/12 + 1100·194.9² = 4.18 × 10⁷ mm⁴
web: 14·330³/12 + 4620·24.91² = 4.479 × 10⁷ mm⁴
bottom flange: 160·14³/12 + 2240·147.1² = 4.85 × 10⁷ mm⁴
Ix = 4.18 × 10⁷ + 4.479 × 10⁷ + 4.85 × 10⁷
Ix = 1.351 × 10⁸ mm⁴ = 135.1 × 10⁶ mm⁴

Answer

Ix = 135.1 × 10⁶ mm⁴

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