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 scalar projection compb a of a = (6, −3, −6) onto b = (−2, 1, −4), that is, the component of a in the direction of b.

a = (6, −3, −6)b = (−2, 1, −4)
compb a =
2.Vectors: dot & cross productHard
xyzabc

Find the volume V of the parallelepiped whose edges from one corner are a = (−4, −1, −5), b = (−2, 2, 4) and c = (−5, −4, 4).

a = (−4, −1, −5)b = (−2, 2, 4)c = (−5, −4, 4)
V =
3.Beam support reactionsMedium
P1​ = 10 kNP2​ = 10 kNABRA​RB​ = ?1 m4 m1 m

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

L = 6 mP1 = 10 kN at 1 mP2 = 10 kN at 5 m
RB = kN
4.Beam support reactionsHard
w0​ = 15 kN/mP = 15 kNABMA​ = ?2 m3 m

The cantilever beam is fixed to the wall at A. It carries a linearly varying load that is 15 kN/m at the wall and falls to zero at the free end B, plus a point load P at 2 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 5 mw0 = 15 kN/mP = 15 kN at 2 m
MA = kN·m
5.Truss: method of jointsMedium
ABCDEFGH10 kN35 kN30 kN25 kN40 kN4 × 3 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: 10 kN ↓C: 35 kN ↓D: 30 kN ↓F: 25 kN ↓H: 40 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 FC
  13. 13member HC
6.Truss: method of jointsHard
ABBCACACB30 kN5 kN6 m1 m3 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 = 3 mB is 1 m from Avertical load = 30 kNhorizontal load = 5 kN →
FAC = kN
7.Frames & machinesMedium
20 kN6 m1 m2.6 mABCDE

The A-frame shown stands on a pin at A and a roller at B, 6 m apart. The legs meet at the pin C, 3.6 m high, and the horizontal tie DE is 1 m above the ground. A load of 20 kN acts at C. Find the magnitude of the force C that the pin C exerts on leg BC.

P = 20 kNAB = 6 mheight of C = 3.6 mheight of DE = 1 m
C = kN
8.Frames & machinesHard
w = 2 kN/m6 kN1.2 m0.8 m1.2 mABCD

The beam AB of the wall bracket shown is pinned at A and propped by the strut CD (C is 1.2 m below A). The beam carries a uniform load of 2 kN/m over its full length and a point load of 6 kN at its free end B. Find the force FCD in the strut.

w = 2 kN/mP = 6 kNAD = 1.2 mAB = 2 mAC = 1.2 m
FCD = kN
9.Shear force & bending momentMedium
w = 10 kN/mABsection1 m4 m

Find the shear force Vx at the section x = 1 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mw = 10 kN/m from 0 to 5 mx = 1 m
Vx = kN
10.Shear force & bending momentHard
12 kN/m35 kN10 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.

35 kN @ 12 m10 kN @ 2 m12 kN/m, 0–8 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
1403022018xdimensions in mm

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

bf = 140 mmtf = 30 mmtw = 18 mmhw = 220 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
160201808xM = 20 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 20 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 160 mmtf = 20 mmtw = 8 mmhw = 180 mmM = 20 kN·m
σtop = MPa

3Solutions

1.Vectors: dot & cross product

Answer: compb a = 1.964

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 = 6·(−2) + (−3)·1 + (−6)·(−4) = 9

Length of b

|b| = √((−2)² + 1² + (−4)²) = 4.583

Scalar projection

compb a = a·b/|b| = 9/4.583 = 1.964

Answer

compb a = 1.964
2.Vectors: dot & cross product

Answer: V = 174

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 = 2·4 − 4·(−4) = 24
(b × c)y = bzcx − bxcz = 4·(−5) − (−2)·4 = −12
(b × c)z = bxcy − bycx = (−2)·(−4) − 2·(−5) = 18

Dot product with a

a·(b × c) = (−4)·24 + (−1)·(−12) + (−5)·18 = −174
V = |−174| = 174

Answer

V = 174
3.Beam support reactions

Answer: RB = 10 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​ = 10 kNABRA​RB​1 m4 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·6 = 10·1 + 10·5
RB = 60/6 = 10 kN
ΣFy = 0: RA = 20 − 10 = 10 kN

Answer

RB = 10 kN
4.Beam support reactions

Answer: MA = 92.5 kN·m

Cantilever equilibrium: a fixed support can push up and also resist rotation, so it gives a vertical reaction RA and a reaction moment MA. ΣFy = 0 gives RA, and moments about the wall give MA = Σ(load × distance from the wall). A distributed load acts as its resultant at the centroid of the load diagram.

Resultant of the triangular load

W = ½·15·5 = 37.5 kN
x̄ = L/3 = 1.667 m

Moment about the wall

MA = W·x̄ + P·a = 37.5·1.667 + 15·2 = 92.5 kN·m

Answer

MA = 92.5 kN·m
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 G

FG and GH 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: 45.94 kN (T), BC: 45.94 kN (T), CD: 59.06 kN (T), DE: 59.06 kN (T), FG: 65.62 kN (C), GH: 65.62 kN (C), AF: 76.56 kN (C), HE: 98.44 kN (C), BF: 10 kN (T), CG: 0, DH: 30 kN (T), FC: 32.81 kN (T), HC: 10.94 kN (T)

Answer

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

Answer: FAC = 12.5 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.

ABBCACACB30 kN5 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 30·1 + 5·3 → Cy = 7.5 kN
ΣFy = 0: Ay = 30 − 7.5 = 22.5 kN
ΣFx = 0: Ax = −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 = 3/5.831 = 0.5145, cos γ = 5/5.831 = 0.8575
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −7.5/0.5145 = −14.58 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−14.58)·0.8575 = 12.5 kN

Answer

FAC = 12.5 kN (tension)
7.Frames & machines

Answer: C = 15.27 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.

Tie force from leg BC

By = 10 kN
T = 10·3/2.6 = 11.54 kN

Components of the pin force on BC

Cx = T = 11.54 kN, Cy = −By = −10 kN

Magnitude

C = √(11.54² + 10²) = 15.27 kN

Answer

C = 15.27 kN
8.Frames & machines

Answer: FCD = 18.86 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 = 4 kN at 1 m

Moments about A for the beam

FCD·0.7071·1.2 = 4·1 + 6·2 = 16 kN·m
FCD = 18.86 kN

Answer

FCD = 18.86 kN
9.Shear force & bending moment

Answer: Vx = 15 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 = 10·5 = 50 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 10·5·2.5
RB = 125/5 = 25 kN
ΣFy = 0: RA = 50 − 25 = 25 kN
w = 10 kN/mABRA​ = 25RB​ = 25section1 m4 m

Cut at x = 1 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 = 25 − 10·1 = 15 kN

Answer

Vx = 15 kN
10.Shear force & bending moment

Answer: E (x = 8 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 = 38 kN, R2 = 103 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 = 52, MC = 36, MD = −28, ME = −140 kN·m, MF = −70, MG = 0

Answer

Mark E: ME = −140 kN·m
11.Centroid & second moment of area

Answer: Ix = 48.13 × 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 = 140·30 = 4200 mm², yf = 220 + 30/2 = 235 mm
web: Aw = 18·220 = 3960 mm², yw = 220/2 = 110 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4200·235 + 3960·110)/8160 = 174.3 mm

Parallel-axis theorem

flange: 140·30³/12 + 4200·(235 − 174.3)² = 1.577 × 10⁷ mm⁴
web: 18·220³/12 + 3960·(110 − 174.3)² = 3.236 × 10⁷ mm⁴
Ix = 1.577 × 10⁷ + 3.236 × 10⁷ = 4.813 × 10⁷ mm⁴ = 48.13 × 10⁶ mm⁴

Answer

Ix = 48.13 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 58.93 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 = 160·20 = 3200 mm², yf = 180 + 20/2 = 190 mm
web: Aw = 8·180 = 1440 mm², yw = 180/2 = 90 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3200·190 + 1440·90)/4640 = 159 mm

Parallel-axis theorem

flange: 160·20³/12 + 3200·(190 − 159)² = 3.189 × 10⁶ mm⁴
web: 8·180³/12 + 1440·(90 − 159)² = 1.074 × 10⁷ mm⁴
Ix = 3.189 × 10⁶ + 1.074 × 10⁷ = 1.393 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 200 − 159 = 41.03 mm
σ = M·y/I = 2 × 10⁷·41.03/1.393 × 10⁷ = 58.93 MPa

Answer

σtop = 58.93 MPa

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