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 = (−15, 15, −20) N acts on an object while it moves in a straight line from point A(1, 0, −5) to point B(2, 3, 0). Coordinates are in metres. Find the work W done by the force.

F = (−15, 15, −20) NA(1, 0, −5) mB(2, 3, 0) m
W = J
2.Vectors: dot & cross productHard
xyzabc

Find the volume V of the parallelepiped whose edges from one corner are a = (−5, −5, 0), b = (4, −5, −1) and c = (−4, 5, 3).

a = (−5, −5, 0)b = (4, −5, −1)c = (−4, 5, 3)
V =
3.Beam support reactionsMedium
w0​ = 4 kN/mABRA​ = ?8 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that falls from 4 kN/m at A to zero at B. Find the vertical support reaction RA.

L = 8 mw0 = 4 kN/m
RA = kN
4.Beam support reactionsHard
w = 3 kN/mP = 60 kNABRA​ = ?RB​1.5 m0.5 m2 m2 m

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

L = 6 mP = 60 kN at 1.5 mw = 3 kN/m from 2 to 4 m
RA = kN
5.Truss: method of jointsMedium
ABCDEFGH20 kN20 kN30 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.

F: 20 kN ↓G: 20 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
6.Truss: method of jointsHard
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
7.Frames & machinesMedium
8 kN0.75 m0.75 m0.75 mABCD

A horizontal beam AB is pinned to a wall at A and propped by the strut CD, pinned to the wall at C, 0.75 m below A. A load of 8 kN hangs at B. Neglect the weights. Find the magnitude of the pin force A on the beam at A.

P = 8 kNAD = 0.75 mAB = 1.5 mAC = 0.75 m
A = kN
8.Frames & machinesHard
2 kN1.5 kN3 m1 mABC

A uniform horizontal boom AB of weight 1.5 kN is pinned to a wall at A and held by a cable from its end B to the point C on the wall, 1 m above A. A load of 2 kN hangs at B. Find the tension T in the cable.

W = 2 kNWb = 1.5 kNAB = 3 mAC = 1 m
T = kN
9.Shear force & bending momentMedium
w = 12 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 = 12 kN/m from 0 to 8 mx = 7 m
Mx = kN·m
10.Shear force & bending momentHard
w = 3 kN/mABC6 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 = 7 mw = 3 kN/m from 0 to 7 msupports at x = 0 and x = 6 m
Mmax = kN·m
11.Centroid & second moment of areaMedium
220180t = 12xdimensions in mm

A channel section lies with its open side up: a base plate 220 mm wide with two upright legs, 180 mm high overall. Base and legs are all 12 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.

b = 220 mmh = 180 mmt = 12 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2201012014xsagging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 35 MPa in tension and 120 MPa in compression. Find the largest sagging bending moment Mallow the beam can carry.

bf = 220 mmtf = 10 mmtw = 14 mmhw = 120 mmσt,allow = 35 MPaσc,allow = 120 MPa
Mallow = kN·m

3Solutions

1.Vectors: dot & cross product

Answer: W = −70 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, 3, 0) − (1, 0, −5) = (1, 3, 5) m

Work

W = F·d = (−15)·1 + 15·3 + (−20)·5 = −70 J

Answer

W = −70 J

Negative work: the force acts mostly against the motion.

2.Vectors: dot & cross product

Answer: V = 90

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 b × c

(b × c)x = bycz − bzcy = (−5)·3 − (−1)·5 = −10
(b × c)y = bzcx − bxcz = (−1)·(−4) − 4·3 = −8
(b × c)z = bxcy − bycx = 4·5 − (−5)·(−4) = 0

Dot product with a

a·(b × c) = (−5)·(−10) + (−5)·(−8) + 0·0 = 90
V = |90| = 90

Answer

V = 90
3.Beam support reactions

Answer: RA = 10.67 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 = ½·4·8 = 16 kN
x̄ = L/3 = 2.667 m

Equilibrium

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

ΣMA = 0: RB·8 = 16·2.667
RB = 5.333 kN
RA = 16 − 5.333 = 10.67 kN

Answer

RA = 10.67 kN
4.Beam support reactions

Answer: RA = 48 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 = 60 kNABRA​RB​1.5 m0.5 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 = 3 m
ΣMA = 0: RB·6 = 60·1.5 + 3·2·3
RB = 108/6 = 18 kN
ΣFy = 0: RA = 66 − 18 = 48 kN

Answer

RA = 48 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: 32.5 kN (T), BC: 45 kN (T), CD: 45 kN (T), DE: 37.5 kN (T), FG: 32.5 kN (C), GH: 37.5 kN (C), AF: 45.96 kN (C), HE: 53.03 kN (C), BF: 12.5 kN (T), CG: 0, DH: 7.5 kN (T), BG: 17.68 kN (C), DG: 10.61 kN (C)

Answer

Zero-force member: CG
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: 7.5 kN (C), BC: 5 kN (C), CD: 5 kN (C), DE: 2.5 kN (C), FG: 2.5 kN (C), GH: 7.5 kN (C), AF: 3.536 kN (C), HE: 3.536 kN (T), 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
7.Frames & machines

Answer: A = 17.89 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.

Strut force

FCD = 8·1.5/(0.7071·0.75) = 22.63 kN

Components at A

Ax = FCD·cos α = 16 kN (towards the wall)
Ay = 8 − FCD·sin α = −8 kN

Magnitude

A = √(16² + −8²) = 17.89 kN

Answer

A = 17.89 kN

A negative Ay means the wall pulls the beam down at A.

8.Frames & machines

Answer: T = 8.696 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.

Cable angle

BC = √(3² + 1²) = 3.162 m, sin β = 0.3162

Moments about A

T·0.3162·3 = 2·3 + 1.5·1.5
T = 8.696 kN

Answer

T = 8.696 kN
9.Shear force & bending moment

Answer: Mx = 42 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 = 12·8 = 96 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 12·8·4
RB = 384/8 = 48 kN
ΣFy = 0: RA = 96 − 48 = 48 kN
w = 12 kN/mABRA​ = 48RB​ = 48section7 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 = 48·7 − 12·7·3.5 = 42 kN·m

Answer

Mx = 42 kN·m
10.Shear force & bending moment

Answer: Mmax = 12.76 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 = 3·7 = 21 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·6 = 3·7·3.5
RB = 73.5/6 = 12.25 kN
ΣFy = 0: RA = 21 − 12.25 = 8.75 kN

Zero shear

RA − w·x0 = 0 → x0 = 8.75/3 = 2.917 m

Maximum sagging moment

Mmax = RA·x0 − w·x0²/2 = RA²/(2w) = 8.75²/(2·3) = 12.76 kN·m

Answer

Mmax = 12.76 kN·m
11.Centroid & second moment of area

Answer: Ix = 22.44 × 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 rectangles

Take the base at full width and the two legs above it (height h − t), so nothing is counted twice.

base: A1 = 220·12 = 2640 mm², y1 = 6 mm
two legs: A2 = 2·12·168 = 4032 mm², y2 = 12 + 168/2 = 96 mm

Centroid

ȳ = (2640·6 + 4032·96)/6672 = 60.39 mm

Parallel-axis theorem

base: 220·12³/12 + 2640·(6 − 60.39)² = 7.841 × 10⁶ mm⁴
two legs: 2·12·168³/12 + 4032·(96 − 60.39)² = 1.46 × 10⁷ mm⁴
Ix = 7.841 × 10⁶ + 1.46 × 10⁷
Ix = 2.244 × 10⁷ mm⁴ = 22.44 × 10⁶ mm⁴

Answer

Ix = 22.44 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 2.189 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 = (2200·125 + 1680·60)/3880 = 96.86 mm
top edge: c = 130 − 96.86 = 33.14 mm

Second moment of area

I = 220·10³/12 + 2200·28.14² + 14·120³/12 + 1680·36.86² = 6.059 × 10⁶ mm⁴

Moment allowed by each edge

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

top edge: M = 120·6.059 × 10⁶/33.14 = 21.94 kN·m
bottom edge: M = 35·6.059 × 10⁶/96.86 = 2.189 kN·m

Governing value

Mallow = min = 2.189 kN·m (bottom edge)

Answer

Mallow = 2.189 kN·m

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