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 = (−4, 6, −5) onto b = (6, 2, −4), that is, the component of a in the direction of b.

a = (−4, 6, −5)b = (6, 2, −4)
compb a =
2.Vectors: dot & cross productHard
xyzabc

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

a = (1, 4, −3)b = (5, 5, −1)c = (−3, −1, 1)
V =
3.Beam support reactionsMedium
w0​ = 12 kN/mP = 60 kNABRB​ = ?3.5 m0.5 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that falls from 12 kN/m at A to zero at B. A point load P also acts at 3.5 m from A. Find the vertical support reaction RB.

L = 4 mw0 = 12 kN/mP = 60 kN at 3.5 m
RB = kN
4.Beam support reactionsHard
w = 12 kN/mP = 15 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 RA.

L = 6 mP = 15 kN at 1 mw = 12 kN/m from 0 to 5 m
RA = kN
5.Truss: method of jointsMedium
ABCDEFGH20 kN30 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.

F: 20 kN ↓G: 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
ABBCACACB10 kN30 kN4 m3 m3 m

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

span = 4 mheight = 3 mB is 3 m from Avertical load = 10 kNhorizontal load = 30 kN →
FBC = kN
7.Frames & machinesMedium
200 NQ = ?10°ABC

In the toggle clamp shown, two equal links AB and BC are pinned together at B, and each makes 10° with the line AC. A downward force of 200 N is applied at B. The slider C presses on a workpiece. Neglecting friction and weights, find the horizontal clamping force Q.

F = 200 Nθ = 10°
Q = N
8.Frames & machinesHard
20 kN2 kN4 m2 m0.6 mABCK

The frame shown has pins at A, B and C; A and C are fixed to the ground 4 m apart, and B is 2 m high and 0.6 m to the right of A. Member AB carries a vertical load of 20 kN at K, 0.45 m (horizontally) from A, and a horizontal load of 2 kN to the right acts at B on member AB. Find the size of the horizontal reaction Ax at A.

P = 20 kNQ = 2 kNL = 4 mH = 2 mhorizontal distance A to B = 0.6 mhorizontal distance A to K = 0.45 m
Ax = kN
9.Shear force & bending momentMedium
M0​ = 45 kN·mAB3.5 m2.5 m

The simply supported beam carries a clockwise couple M0 = 45 kN·m at x = 3.5 m from A, and no other load. Find the bending moment Mx just to the left of the couple. Use sagging moments positive and upward shear on the left face positive.

L = 6 mM0 = 45 kN·m clockwise, at 3.5 m
Mx = kN·m
10.Shear force & bending momentHard
w = 8 kN/mP = 40 kNABsection2.5 m1 m0.5 m

Find the bending moment Mx at the section x = 3.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mP = 40 kN at 2.5 mw = 8 kN/m from 0 to 4 mx = 3.5 m
Mx = kN·m
11.Centroid & second moment of areaMedium
150 mm300 mm120 mmØ40xIx​ = ?

A 150 mm × 300 mm plate has a circular hole of diameter 40 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 = 150 mmh = 300 mmd = 40 mmhole centre: y = 120 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1802526018xsagging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 40 MPa in tension and 150 MPa in compression. Find the largest sagging bending moment Mallow the beam can carry.

bf = 180 mmtf = 25 mmtw = 18 mmhw = 260 mmσt,allow = 40 MPaσc,allow = 150 MPa
Mallow = kN·m

3Solutions

1.Vectors: dot & cross product

Answer: compb a = 1.069

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 = (−4)·6 + 6·2 + (−5)·(−4) = 8

Length of b

|b| = √(6² + 2² + (−4)²) = 7.483

Scalar projection

compb a = a·b/|b| = 8/7.483 = 1.069

Answer

compb a = 1.069
2.Vectors: dot & cross product

Answer: V = 34

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 = 5·1 − (−1)·(−1) = 4
(b × c)y = bzcx − bxcz = (−1)·(−3) − 5·1 = −2
(b × c)z = bxcy − bycx = 5·(−1) − 5·(−3) = 10

Dot product with a

a·(b × c) = 1·4 + 4·(−2) + (−3)·10 = −34
V = |−34| = 34

Answer

V = 34
3.Beam support reactions

Answer: RB = 60.5 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.

Resultant of the triangular load

W = ½·12·4 = 24 kN
x̄ = L/3 = 1.333 m

Equilibrium

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

ΣMA = 0: RB·4 = 24·1.333 + 60·3.5
RB = 60.5 kN
RA = 84 − 60.5 = 23.5 kN

Answer

RB = 60.5 kN
4.Beam support reactions

Answer: RA = 47.5 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.

w = 12 kN/mP = 15 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.

UDL resultant: W = w·ℓ = 12·5 = 60 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·6 = 15·1 + 12·5·2.5
RB = 165/6 = 27.5 kN
ΣFy = 0: RA = 75 − 27.5 = 47.5 kN

Answer

RA = 47.5 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: 22.5 kN (T), BC: 30 kN (T), CD: 30 kN (T), DE: 15 kN (T), FG: 22.5 kN (C), GH: 15 kN (C), AF: 37.5 kN (C), HE: 25 kN (C), BF: 10 kN (T), CG: 0, DH: 20 kN (T), BG: 12.5 kN (C), DG: 25 kN (C)

Answer

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

Answer: FBC = −31.62 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 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·4 = 10·3 + 30·3 → Cy = 30 kN
ΣFy = 0: Ay = 10 − 30 = −20 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 = 3/3.162 = 0.9487, cos γ = 1/3.162 = 0.3162
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −30/0.9487 = −31.62 kN

Answer

FBC = −31.62 kN (compression)
7.Frames & machines

Answer: Q = 567.1 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 10° = 200
Flink = 575.9 N

Clamping force

Q = Flink·cos 10° = 200/(2·tan 10°) = 567.1 N

Answer

Q = 567.1 N

The force ratio Q/F = 2.836 grows without limit as the links straighten.

8.Frames & machines

Answer: Ax = 3.525 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.

Direction of BC

BC = 3.945 m, cos = 0.8619, sin = 0.507

Whole frame: moments about A

FBC·0.507·4 = 20·0.45 + 2·2
FBC = 6.41 kN

Horizontal balance

Ax + 2 − 6.41·0.8619 = 0
Ax = 3.525 kN → |Ax| = 3.525 kN

Answer

Ax = 3.525 kN

Ax points to the right.

9.Shear force & bending moment

Answer: Mx = −26.25 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. An applied couple makes the bending moment diagram jump by the size of the couple.

Support reactions

Moments about A, counter-clockwise positive: RB·L − M0 = 0. Vertical balance: RA + RB = 0.

RB = M0/L = 45/6 = 7.5 kN (upward)
RA = −RB = −7.5 kN (downward)

Cut just left of the couple

The left part contains only RA.

Mx = RA·a = −7.5·3.5 = −26.25 kN·m

Answer

Mx = −26.25 kN·m
10.Shear force & bending moment

Answer: Mx = 19.5 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.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 8·4 = 32 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 40·2.5 + 8·4·2
RB = 164/4 = 41 kN
ΣFy = 0: RA = 72 − 41 = 31 kN
w = 8 kN/mP = 40 kNABRA​ = 31RB​ = 41section2.5 m1 m0.5 m

Cut at x = 3.5 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 = 31·3.5 − 40·(3.5 − 2.5) − 8·3.5·1.75 = 19.5 kN·m

Answer

Mx = 19.5 kN·m
11.Centroid & second moment of area

Answer: Ix = 336.2 × 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 = (45000·150 − 1257·120)/(45000 − 1257) = 150.9 mm

Full plate about ȳ

150·300³/12 + 45000·−0.8618² = 337.5 × 10⁶ mm⁴

Hole about ȳ

π·40⁴/64 + 1257·−30.86² = 1.323 × 10⁶ mm⁴

Subtract

Ix = 336.2 × 10⁶ mm⁴

Answer

Ix = 336.2 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 14.65 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 = (4500·272.5 + 4680·130)/9180 = 199.9 mm
top edge: c = 285 − 199.9 = 85.15 mm

Second moment of area

I = 180·25³/12 + 4500·72.65² + 18·260³/12 + 4680·69.85² = 7.318 × 10⁷ mm⁴

Moment allowed by each edge

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

top edge: M = 150·7.318 × 10⁷/85.15 = 128.9 kN·m
bottom edge: M = 40·7.318 × 10⁷/199.9 = 14.65 kN·m

Governing value

Mallow = min = 14.65 kN·m (bottom edge)

Answer

Mallow = 14.65 kN·m

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