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
xyzdFAB

A constant force F = (−20, 20, 15) N acts on an object while it moves in a straight line from point A(3, −4, 2) to point B(2, −5, 3). Coordinates are in metres. Find the work W done by the force.

F = (−20, 20, 15) NA(3, −4, 2) mB(2, −5, 3) m
W = J
2.Vectors: dot & cross productHard
xyzab

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

a = (−4, 4, −4)b = (4, 1, 2)n̂z > 0
n̂x =
3.Beam support reactionsMedium
P1​ = 55 kNP2​ = 45 kNABRA​RB​ = ?2 m2 m1 m

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

L = 5 mP1 = 55 kN at 2 mP2 = 45 kN at 4 m
RB = kN
4.Beam support reactionsHard
w = 12 kN/mP = 25 kNABRA​ = ?RB​1 m1 m2 m1 m

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

L = 5 mP = 25 kN at 4 mw = 12 kN/m from 1 to 2 m
RA = kN
5.Truss: method of jointsMedium
ABCDEFGH10 kN4 × 3 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.

H: 10 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
ABBCACACB25 kN30 kN5 m4 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 4 m from Avertical load = 25 kNhorizontal load = 30 kN ←
FAC = kN
7.Frames & machinesMedium
20 kN5 m3 m3 mABCK

The frame shown has pins at A, B and C; A and C are fixed to the ground 5 m apart, and B is 3 m above the ground and 3 m to the right of A. A vertical load of 20 kN acts on member AB at K, 2.25 m (horizontally) from A. Find the force FBC in member BC.

P = 20 kNL = 5 mH = 3 mhorizontal distance A to B = 3 mhorizontal distance A to K = 2.25 m
FBC = kN
8.Frames & machinesHard
w = 2 kN/m10 kN1.2 m1.3 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 2 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 = 2 kN/mP = 10 kNAD = 1.2 mAB = 2.5 mAC = 0.6 m
FCD = kN
9.Shear force & bending momentMedium
w = 6 kN/mABsection7 m1 m

Find the bending moment Mx at the section x = 7 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mw = 6 kN/m from 0 to 8 mx = 7 m
Mx = kN·m
10.Shear force & bending momentHard
w = 8 kN/mABC8 m1 m

The beam rests on a pin at A and a roller at B and overhangs B by 1 m to the free end C. A uniformly distributed load w acts over the whole length A–C. Find the maximum sagging bending moment Mmax between the supports.

L = 9 mw = 8 kN/m from 0 to 9 msupports at x = 0 and x = 8 m
Mmax = kN·m
11.Centroid & second moment of areaMedium
2603010018xdimensions in mm

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

bf = 260 mmtf = 30 mmtw = 18 mmhw = 100 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1001012012xM = 15 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 15 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 100 mmtf = 10 mmtw = 12 mmhw = 120 mmM = 15 kN·m
σtop = MPa

3Solutions

1.Vectors: dot & cross product

Answer: W = 15 J

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.

Displacement

d = B − A = (2, −5, 3) − (3, −4, 2) = (−1, −1, 1) m

Work

W = F·d = (−20)·(−1) + 20·(−1) + 15·1 = 15 J

Answer

W = 15 J
2.Vectors: dot & cross product

Answer: n̂x = −0.4867

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 = 4·2 − (−4)·1 = 12
(a × b)y = azbx − axbz = (−4)·4 − (−4)·2 = −8
(a × b)z = axby − aybx = (−4)·1 − 4·4 = −20

Normalise

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

|a × b| = √(12² + (−8)² + (−20)²) = 24.66
n̂ = −(12, −8, −20)/24.66 = (−0.4867, 0.3244, 0.8111)
n̂x = −0.4867

Answer

n̂x = −0.4867
3.Beam support reactions

Answer: RB = 58 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​ = 55 kNP2​ = 45 kNABRA​RB​2 m2 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.

ΣMA = 0: RB·5 = 55·2 + 45·4
RB = 290/5 = 58 kN
ΣFy = 0: RA = 100 − 58 = 42 kN

Answer

RB = 58 kN
4.Beam support reactions

Answer: RA = 13.4 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 = 12 kN/mP = 25 kNABRA​RB​1 m1 m2 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 = 12·1 = 12 kN, acting at x̄ = 1.5 m
ΣMA = 0: RB·5 = 25·4 + 12·1·1.5
RB = 118/5 = 23.6 kN
ΣFy = 0: RA = 37 − 23.6 = 13.4 kN

Answer

RA = 13.4 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: 2.5 kN (T), BC: 5 kN (T), CD: 5 kN (T), DE: 7.5 kN (T), FG: 2.5 kN (C), GH: 7.5 kN (C), AF: 3.536 kN (C), HE: 10.61 kN (C), BF: 2.5 kN (T), CG: 0, DH: 2.5 kN (C), BG: 3.536 kN (C), DG: 3.536 kN (T)

Answer

Zero-force member: CG
6.Truss: method of joints

Answer: FAC = 4 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.

ABBCACACB25 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 25·4 − 30·2 → Cy = 8 kN
ΣFy = 0: Ay = 25 − 8 = 17 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 = 2/2.236 = 0.8944, cos γ = 1/2.236 = 0.4472
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −8/0.8944 = −8.944 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−8.944)·0.4472 = 4 kN

Answer

FAC = 4 kN (tension)
7.Frames & machines

Answer: FBC = 10.82 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 = √(2² + 3²) = 3.606 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·(3/3.606)·5 = 20·2.25
FBC = 10.82 kN (compression)

Answer

FBC = 10.82 kN
8.Frames & machines

Answer: FCD = 58.23 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 = 2·2.5 = 5 kN at 1.25 m

Moments about A for the beam

FCD·0.4472·1.2 = 5·1.25 + 10·2.5 = 31.25 kN·m
FCD = 58.23 kN

Answer

FCD = 58.23 kN
9.Shear force & bending moment

Answer: Mx = 21 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 = 6·8 = 48 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 6·8·4
RB = 192/8 = 24 kN
ΣFy = 0: RA = 48 − 24 = 24 kN
w = 6 kN/mABRA​ = 24RB​ = 24section7 m1 m

Cut at x = 7 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 = 24·7 − 6·7·3.5 = 21 kN·m

Answer

Mx = 21 kN·m
10.Shear force & bending moment

Answer: Mmax = 62.02 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, including the load on the overhang.

UDL resultant: W = w·ℓ = 8·9 = 72 kN, acting at x̄ = 4.5 m
ΣMA = 0: RB·8 = 8·9·4.5
RB = 324/8 = 40.5 kN
ΣFy = 0: RA = 72 − 40.5 = 31.5 kN

Zero shear

RA − w·x0 = 0 → x0 = 31.5/8 = 3.938 m

Maximum sagging moment

Mmax = RA·x0 − w·x0²/2 = RA²/(2w) = 31.5²/(2·8) = 62.02 kN·m

Answer

Mmax = 62.02 kN·m
11.Centroid & second moment of area

Answer: Ix = 8.264 × 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 = 260·30 = 7800 mm², yf = 100 + 30/2 = 115 mm
web: Aw = 18·100 = 1800 mm², yw = 100/2 = 50 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (7800·115 + 1800·50)/9600 = 102.8 mm

Parallel-axis theorem

flange: 260·30³/12 + 7800·(115 − 102.8)² = 1.744 × 10⁶ mm⁴
web: 18·100³/12 + 1800·(50 − 102.8)² = 6.52 × 10⁶ mm⁴
Ix = 1.744 × 10⁶ + 6.52 × 10⁶ = 8.264 × 10⁶ mm⁴ = 8.264 × 10⁶ mm⁴

Answer

Ix = 8.264 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 153.8 MPa

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 = 100·10 = 1000 mm², yf = 120 + 10/2 = 125 mm
web: Aw = 12·120 = 1440 mm², yw = 120/2 = 60 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (1000·125 + 1440·60)/2440 = 86.64 mm

Parallel-axis theorem

flange: 100·10³/12 + 1000·(125 − 86.64)² = 1.48 × 10⁶ mm⁴
web: 12·120³/12 + 1440·(60 − 86.64)² = 2.75 × 10⁶ mm⁴
Ix = 1.48 × 10⁶ + 2.75 × 10⁶ = 4.23 × 10⁶ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 130 − 86.64 = 43.36 mm
σ = M·y/I = 1.5 × 10⁷·43.36/4.23 × 10⁶ = 153.8 MPa

Answer

σtop = 153.8 MPa

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