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 value of k for which the vectors a = (2, −3, −3) and b = (0, −2, k) are perpendicular.

a = (2, −3, −3)b = (0, −2, k)
k =
2.Vectors: dot & cross productHard
xyzab

The unit vector n̂ is perpendicular to both a = (−2, 2, 1) and b = (4, 2, 1) and has a positive z-component. Find its y-component n̂y.

a = (−2, 2, 1)b = (4, 2, 1)n̂z > 0
n̂y =
3.Beam support reactionsMedium
P1​ = 50 kNP2​ = 25 kNABRA​RB​ = ?2 m0.5 m2.5 m

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

L = 5 mP1 = 50 kN at 2 mP2 = 25 kN at 2.5 m
RB = kN
4.Beam support reactionsHard
P = 20 kN, 30°Q = 15 kNABRA​ = ?2.5 m1 m0.5 m

The simply supported beam has a pin at A and a roller at B. A load P acts at 3.5 m from A, inclined at 30° to the horizontal, and a vertical load Q acts at 2.5 m from A. Find the magnitude of the total reaction force RA at the pin A.

L = 4 mP = 20 kN at 3.5 m, θ = 30°Q = 15 kN at 2.5 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB10 kN5 m3 m2 m

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

span = 5 mheight = 2 mB is 3 m from Avertical load = 10 kN
FAC = kN
6.Truss: method of jointsHard
ABBCACACB55 kN30 kN8 m2 m4 m

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

span = 8 mheight = 4 mB is 2 m from Avertical load = 55 kNhorizontal load = 30 kN ←
FAC = kN
7.Frames & machinesMedium
100 NQ = ?25°ABC

In the toggle clamp shown, two equal links AB and BC are pinned together at B, and each makes 25° 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 = 25°
Q = N
8.Frames & machinesHard
F = ?1500 N5 mmABC

A toggle press has two equal links AB and BC, each 100 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 = 100 mmh = 5 mm
F = N
9.Shear force & bending momentMedium
w = 12 kN/mABsection3 m1 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 = 4 mw = 12 kN/m from 0 to 4 mx = 3 m
Vx = kN
10.Shear force & bending momentHard
55 kN15 kN20 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.

55 kN @ 0 m15 kN @ 12 m20 kN @ 4 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)
11.Centroid & second moment of areaMedium
120 mm200 mm120 mmØ30xIx​ = ?

A 120 mm × 200 mm plate has a circular hole of diameter 30 mm on its vertical centre line, with its centre 120 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 120 mmh = 200 mmd = 30 mmhole centre: y = 120 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
3002018018xsagging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 30 MPa in tension and 120 MPa in compression. Find the largest sagging bending moment Mallow the beam can carry.

bf = 300 mmtf = 20 mmtw = 18 mmhw = 180 mmσt,allow = 30 MPaσc,allow = 120 MPa
Mallow = kN·m

3Solutions

1.Vectors: dot & cross product

Answer: k = 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.

Dot product equals zero

a·b = 2·0 + (−3)·(−2) + (−3)·k = 0
6 + (−3)·k = 0

Solve for k

k = −6/(−3) = 2

Answer

k = 2
2.Vectors: dot & cross product

Answer: n̂y = −0.4472

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 = 2·1 − 1·2 = 0
(a × b)y = azbx − axbz = 1·4 − (−2)·1 = 6
(a × b)z = axby − aybx = (−2)·2 − 2·4 = −12

Normalise

The z-component of a × b is negative, so use −(a × b).

|a × b| = √(0² + 6² + (−12)²) = 13.42
n̂ = −(0, 6, −12)/13.42 = (0, −0.4472, 0.8944)
n̂y = −0.4472

Answer

n̂y = −0.4472
3.Beam support reactions

Answer: RB = 32.5 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​ = 50 kNP2​ = 25 kNABRA​RB​2 m0.5 m2.5 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·5 = 50·2 + 25·2.5
RB = 162.5/5 = 32.5 kN
ΣFy = 0: RA = 75 − 32.5 = 42.5 kN

Answer

RB = 32.5 kN
4.Beam support reactions

Answer: RA = 18.64 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.

Components of P

Pv = 20·sin 30° = 10 kN
Ph = 20·cos 30° = 17.32 kN

Reactions

ΣMA = 0: RB·4 = 10·3.5 + 15·2.5 → RB = 18.13 kN
Ay = 10 + 15 − 18.13 = 6.875 kN
Ax = Ph = 17.32 kN

Resultant at A

RA = √(17.32² + 6.875²) = 18.64 kN

Answer

RA = 18.64 kN
5.Truss: method of joints

Answer: FAC = 6 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.

ABBCACACB10 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 10·3 → Cy = 6 kN
ΣFy = 0: Ay = 10 − 6 = 4 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 = 2/2.828 = 0.7071, cos γ = 2/2.828 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −6/0.7071 = −8.485 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−8.485)·0.7071 = 6 kN

Answer

FAC = 6 kN (tension)
6.Truss: method of joints

Answer: FAC = −1.875 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 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 55·2 − 30·4 → Cy = −1.25 kN
ΣFy = 0: Ay = 55 − −1.25 = 56.25 kN
ΣFx = 0: Ax = 30 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 = 4/7.211 = 0.5547, cos γ = 6/7.211 = 0.8321
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −−1.25/0.5547 = 2.253 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(2.253)·0.8321 = −1.875 kN

Answer

FAC = −1.875 kN (compression)
7.Frames & machines

Answer: Q = 107.2 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 25° = 100
Flink = 118.3 N

Clamping force

Q = Flink·cos 25° = 100/(2·tan 25°) = 107.2 N

Answer

Q = 107.2 N

The force ratio Q/F = 1.072 grows without limit as the links straighten.

8.Frames & machines

Answer: F = 150.2 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 = 5/100 = 0.05, θ = 2.866°

Link force

Flink = Q/cos θ = 1502 N

Force at B

F = 2·Flink·sin θ = 2·1500·tan θ = 150.2 N

Answer

F = 150.2 N
9.Shear force & bending moment

Answer: Vx = −12 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 = 12·4 = 48 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 12·4·2
RB = 96/4 = 24 kN
ΣFy = 0: RA = 48 − 24 = 24 kN
w = 12 kN/mABRA​ = 24RB​ = 24section3 m1 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 = 24 − 12·3 = −12 kN

Answer

Vx = −12 kN
10.Shear force & bending moment

Answer: B (x = 2 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 = 76.67 kN, R2 = 13.33 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 = −110 kN·m, MC = −66.67, MD = −63.33, ME = −60, MF = −30, MG = 0

Answer

Mark B: MB = −110 kN·m
11.Centroid & second moment of area

Answer: Ix = 79.67 × 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 = (24000·100 − 706.9·120)/(24000 − 706.9) = 99.39 mm

Full plate about ȳ

120·200³/12 + 24000·0.6069² = 80.01 × 10⁶ mm⁴

Hole about ȳ

π·30⁴/64 + 706.9·20.61² = 0.3399 × 10⁶ mm⁴

Subtract

Ix = 79.67 × 10⁶ mm⁴

Answer

Ix = 79.67 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 5.806 kN·m

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.

Centroid

ȳ = (6000·190 + 3240·90)/9240 = 154.9 mm
top edge: c = 200 − 154.9 = 45.06 mm

Second moment of area

I = 300·20³/12 + 6000·35.06² + 18·180³/12 + 3240·64.94² = 2.999 × 10⁷ mm⁴

Moment allowed by each edge

Sagging: the top is in compression, the bottom in tension.

top edge: M = 120·2.999 × 10⁷/45.06 = 79.85 kN·m
bottom edge: M = 30·2.999 × 10⁷/154.9 = 5.806 kN·m

Governing value

Mallow = min = 5.806 kN·m (bottom edge)

Answer

Mallow = 5.806 kN·m

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