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 = (5, 6, 3) and b = (3, 3, −1), in degrees.

a = (5, 6, 3)b = (3, 3, −1)
θ = °
2.Vectors: dot & cross productHard
xyzab

The unit vector n̂ is perpendicular to both a = (4, −3, 5) and b = (0, 4, 2) and has a positive z-component. Find its y-component n̂y.

a = (4, −3, 5)b = (0, 4, 2)n̂z > 0
n̂y =
3.Beam support reactionsMedium
P1​ = 10 kNP2​ = 40 kNABRA​ = ?RB​1 m7 m2 m

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

L = 10 mP1 = 10 kN at 1 mP2 = 40 kN at 8 m
RA = kN
4.Beam support reactionsHard
w = 10 kN/mP = 65 kNADCRD​ = ?3 m1.5 m1.5 m

A compound beam is fixed to the wall at A, has an internal hinge at C (3 m from A) and rests on a roller at D (6 m from A). It carries a point load P at 4.5 m from A, a uniformly distributed load w on the whole part CD. Find the reaction RD at the roller.

AC = 3 mAD = 6 mP = 65 kN at 4.5 mw = 10 kN/m from 3 to 6 m
RD = kN
5.Truss: method of jointsMedium
ABBCACACB45 kN8 m7 m3 m

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

span = 8 mheight = 3 mB is 7 m from Avertical load = 45 kN
FBC = kN
6.Truss: method of jointsHard
ABBCACACB40 kN5 kN5 m2 m3 m

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

span = 5 mheight = 3 mB is 2 m from Avertical load = 40 kNhorizontal load = 5 kN ←
FAB = kN
7.Frames & machinesMedium
15 kN3 m3 m1.35 mABCK

The frame shown has pins at A, B and C; A and C are fixed to the ground 3 m apart, and B is 3 m above the ground and 1.35 m to the right of A. A vertical load of 15 kN acts on member AB at K, 0.675 m (horizontally) from A. Find the force FBC in member BC.

P = 15 kNL = 3 mH = 3 mhorizontal distance A to B = 1.35 mhorizontal distance A to K = 0.675 m
FBC = kN
8.Frames & machinesHard
w = 1.5 kN/m15 kN0.5 m1 m0.6 mABCD

The beam AB of the wall bracket shown is pinned at A and propped by the strut CD (C is 0.6 m below A). The beam carries a uniform load of 1.5 kN/m over its full length and a point load of 15 kN at its free end B. Find the force FCD in the strut.

w = 1.5 kN/mP = 15 kNAD = 0.5 mAB = 1.5 mAC = 0.6 m
FCD = kN
9.Shear force & bending momentMedium
w = 8 kN/mP = 75 kNAB1.5 m1 m

The cantilever is fixed at A. It carries a uniformly distributed load w over its whole length and a point load P at 1.5 m from A. Find the bending moment MA at the fixed support A. Use sagging moments positive and upward shear on the left face positive.

L = 2.5 mP = 75 kN at 1.5 mw = 8 kN/m from 0 to 2.5 m
MA = kN·m
10.Shear force & bending momentHard
4 kN/m40 kN45 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 @ 0 m45 kN @ 12 m4 kN/m, 2–10 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
2802524014xdimensions in mm

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

bf = 280 mmtf = 25 mmtw = 14 mmhw = 240 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
100 mm150 mm90 mm50 × 20xIx​ = ?

A 100 mm × 150 mm plate has a rectangular cut-out 50 mm wide and 20 mm high, centred on the vertical centre line with its centre 90 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 100 mmh = 150 mmcut-out: 50 × 20 mmhole centre: y = 90 mm
Ix = × 10⁶ mm⁴

3Solutions

1.Vectors: dot & cross product

Answer: θ = 34.65 °

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 = 5·3 + 6·3 + 3·(−1) = 30

Magnitudes

|a| = √(5² + 6² + 3²) = 8.367
|b| = √(3² + 3² + (−1)²) = 4.359

Angle

cos θ = 30/(8.367·4.359) = 0.8226
θ = arccos(0.8226) = 34.65°

Answer

θ = 34.65°
2.Vectors: dot & cross product

Answer: n̂y = −0.2535

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 = (−3)·2 − 5·4 = −26
(a × b)y = azbx − axbz = 5·0 − 4·2 = −8
(a × b)z = axby − aybx = 4·4 − (−3)·0 = 16

Normalise

The z-component of a × b is already positive.

|a × b| = √((−26)² + (−8)² + 16²) = 31.56
n̂ = (−26, −8, 16)/31.56 = (−0.8238, −0.2535, 0.507)
n̂y = −0.2535

Answer

n̂y = −0.2535
3.Beam support reactions

Answer: RA = 17 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​ = 40 kNABRA​RB​1 m7 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.

ΣMA = 0: RB·10 = 10·1 + 40·8
RB = 330/10 = 33 kN
ΣFy = 0: RA = 50 − 33 = 17 kN

Answer

RA = 17 kN
4.Beam support reactions

Answer: RD = 47.5 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. An internal hinge cannot carry a bending moment, which gives one extra equation: the moment about the hinge of the forces on either side is zero.

Part CD

The hinge has no moment, so moments about C on CD alone must balance.

W = 10·3 = 30 kN at 1.5 m from C
ΣMC = 0: RD·3 = 65·1.5 + 30·1.5
RD = 47.5 kN
VC = 95 − 47.5 = 47.5 kN

Answer

RD = 47.5 kN
5.Truss: method of joints

Answer: FBC = −41.5 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·8 = 45·7 → Cy = 39.38 kN
ΣFy = 0: Ay = 45 − 39.38 = 5.625 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 = 3/3.162 = 0.9487, cos γ = 1/3.162 = 0.3162
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −39.38/0.9487 = −41.5 kN

Answer

FBC = −41.5 kN (compression)
6.Truss: method of joints

Answer: FAB = −32.45 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.

ABBCACACB40 kN5 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 40·2 − 5·3 → Cy = 13 kN
ΣFy = 0: Ay = 40 − 13 = 27 kN
ΣFx = 0: Ax = 5 kN

Joint A

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

sin α = 3/3.606 = 0.8321
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −27/0.8321 = −32.45 kN

Answer

FAB = −32.45 kN (compression)
7.Frames & machines

Answer: FBC = 3.852 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.

Two-force member BC

BC = √(1.65² + 3²) = 3.424 m

Whole frame: moments about A

The ground pushes on BC at C along CB; its horizontal component passes through A, only the vertical one has a moment.

FBC·(3/3.424)·3 = 15·0.675
FBC = 3.852 kN (compression)

Answer

FBC = 3.852 kN
8.Frames & machines

Answer: FCD = 62.97 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 = 1.5·1.5 = 2.25 kN at 0.75 m

Moments about A for the beam

FCD·0.7682·0.5 = 2.25·0.75 + 15·1.5 = 24.19 kN·m
FCD = 62.97 kN

Answer

FCD = 62.97 kN
9.Shear force & bending moment

Answer: MA = −137.5 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.

Keep the free-end part

P: −75·1.5 = −112.5 kN·m
w: −8·2.5²/2 = −25 kN·m
MA = −112.5 − 25 = −137.5 kN·m

Answer

MA = −137.5 kN·m

Negative means hogging: tension on the top face.

10.Shear force & bending moment

Answer: F (x = 10 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 = 54.75 kN, R2 = 62.25 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 = −80, MC = −58.5, MD = −53, ME = −63.5, MF = −90 kN·m, MG = 0

Answer

Mark F: MF = −90 kN·m
11.Centroid & second moment of area

Answer: Ix = 56.35 × 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 = 280·25 = 7000 mm², yf = 240 + 25/2 = 252.5 mm
web: Aw = 14·240 = 3360 mm², yw = 240/2 = 120 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (7000·252.5 + 3360·120)/10360 = 209.5 mm

Parallel-axis theorem

flange: 280·25³/12 + 7000·(252.5 − 209.5)² = 1.329 × 10⁷ mm⁴
web: 14·240³/12 + 3360·(120 − 209.5)² = 4.306 × 10⁷ mm⁴
Ix = 1.329 × 10⁷ + 4.306 × 10⁷ = 5.635 × 10⁷ mm⁴ = 56.35 × 10⁶ mm⁴

Answer

Ix = 56.35 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 27.85 × 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 = (15000·75 − 1000·90)/(15000 − 1000) = 73.93 mm

Full plate about ȳ

100·150³/12 + 15000·1.071² = 28.14 × 10⁶ mm⁴

Hole about ȳ

50·20³/12 + 1000·16.07² = 0.2916 × 10⁶ mm⁴

Subtract

Ix = 27.85 × 10⁶ mm⁴

Answer

Ix = 27.85 × 10⁶ mm⁴

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