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

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

For a = (−2, 5, 6) and b = (3, 6, 6), find the y-component (a × b)y of the cross product a × b.

a = (−2, 5, 6)b = (3, 6, 6)
(a × b)y =
3.Beam support reactionsMedium
P1​ = 20 kNP2​ = 25 kNABCRB​ = ?4 m1 m3 m

The beam has a pin at A and a roller at B, 5 m from A, and overhangs B to the free end C. Find the vertical reaction RB, taking upward as positive.

AB = 5 mAC = 8 mP1 = 20 kN at 4 mP2 = 25 kN at 8 m
RB = kN
4.Beam support reactionsHard
w = 10 kN/mP = 60 kNABRA​RB​ = ?1 m0.5 m2.5 m

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

L = 4 mP = 60 kN at 1.5 mw = 10 kN/m from 0 to 1 m
RB = kN
5.Truss: method of jointsMedium
ABBCACACB20 kN8 m3 m3 m

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

span = 8 mheight = 3 mB is 3 m from Avertical load = 20 kN
FAC = kN
6.Truss: method of jointsHard
ABBCACACB50 kN30 kN6 m4 m4 m

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

span = 6 mheight = 4 mB is 4 m from Avertical load = 50 kNhorizontal load = 30 kN →
FAB = kN
7.Frames & machinesMedium
15 kN3 m1.8 m2.7 m0.375 mABCDEK

The A-frame shown stands on a pin at A and a roller at B, 3 m apart, with its apex pin C 4.5 m high and the horizontal tie DE 1.8 m above the ground. A vertical load of 15 kN acts on leg AC at K, 0.375 m (horizontally) from A. Find the tension T in the tie.

P = 15 kNAB = 3 mheight of C = 4.5 mheight of DE = 1.8 mhorizontal distance A to K = 0.375 m
T = kN
8.Frames & machinesHard
F = ?2000 N10 mmABC

A toggle press has two equal links AB and BC, each 150 mm long between pins. The joint B sits 10 mm above the line AC. Which downward force F at B produces a horizontal pressing force of 2000 N at the slider C? Neglect friction and weights.

Q = 2000 NAB = BC = 150 mmh = 10 mm
F = N
9.Shear force & bending momentMedium
w = 2 kN/mABsection9 m1 m

Find the bending moment Mx at the section x = 9 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mw = 2 kN/m from 0 to 10 mx = 9 m
Mx = kN·m
10.Shear force & bending momentHard
w = 10 kN/mABC8 m2 m

The beam rests on a pin at A and a roller at B and overhangs B by 2 m to the free end C. A uniformly distributed load w acts over the whole length A–C. Find the bending moment MB at support B. Use sagging moments positive and upward shear on the left face positive.

L = 10 mw = 10 kN/m from 0 to 10 msupports at x = 0 and x = 8 m
MB = kN·m
11.Centroid & second moment of areaMedium
3002014020xdimensions in mm

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

bf = 300 mmtf = 20 mmtw = 20 mmhw = 140 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1001518020xM = 25 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 25 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 100 mmtf = 15 mmtw = 20 mmhw = 180 mmM = 25 kN·m
σbottom = MPa

3Solutions

1.Vectors: dot & cross product

Answer: θ = 120.4 °

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 = 3·(−5) + 6·(−1) + 1·(−6) = −27

Magnitudes

|a| = √(3² + 6² + 1²) = 6.782
|b| = √((−5)² + (−1)² + (−6)²) = 7.874

Angle

cos θ = −27/(6.782·7.874) = −0.5056
θ = arccos(−0.5056) = 120.4°

Answer

θ = 120.4°
2.Vectors: dot & cross product

Answer: (a × b)y = 30

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, component by component

(a × b)x = aybz − azby = 5·6 − 6·6 = −6
(a × b)y = azbx − axbz = 6·3 − (−2)·6 = 30
(a × b)z = axby − aybx = (−2)·6 − 5·3 = −27

Requested component

(a × b)y = 30

Answer

(a × b)y = 30

Check: a × b is perpendicular to both vectors, so its dot product with a and with b is zero.

3.Beam support reactions

Answer: RB = 56 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.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·5 = 20·4 + 25·8
RB = 280/5 = 56 kN

Vertical equilibrium

RA = 20 + 25 − 56 = −11 kN

Answer

RB = 56 kN

RA is negative: the pin at A has to hold the beam down.

4.Beam support reactions

Answer: RB = 23.75 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 = 10 kN/mP = 60 kNABRA​RB​1 m0.5 m2.5 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 = 10·1 = 10 kN, acting at x̄ = 0.5 m
ΣMA = 0: RB·4 = 60·1.5 + 10·1·0.5
RB = 95/4 = 23.75 kN
ΣFy = 0: RA = 70 − 23.75 = 46.25 kN

Answer

RB = 23.75 kN
5.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.

ABBCACACB20 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 20·3 → Cy = 7.5 kN
ΣFy = 0: Ay = 20 − 7.5 = 12.5 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)
6.Truss: method of joints

Answer: FAB = 4.714 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.

ABBCACACB50 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 50·4 + 30·4 → Cy = 53.33 kN
ΣFy = 0: Ay = 50 − 53.33 = −3.333 kN
ΣFx = 0: Ax = −30 kN

Joint A

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

sin α = 4/5.657 = 0.7071
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −−3.333/0.7071 = 4.714 kN

Answer

FAB = 4.714 kN (tension)
7.Frames & machines

Answer: T = 1.042 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.

Whole frame: moments about A

By = 15·0.375/3 = 1.875 kN

Leg BC: moments about C

1.875·1.5 = T·2.7
T = 1.042 kN

Answer

T = 1.042 kN
8.Frames & machines

Answer: F = 267.3 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).

Link angle

sin θ = 10/150 = 0.06667, θ = 3.823°

Link force

Flink = Q/cos θ = 2004 N

Force at B

F = 2·Flink·sin θ = 2·2000·tan θ = 267.3 N

Answer

F = 267.3 N
9.Shear force & bending moment

Answer: Mx = 9 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 = 2·10 = 20 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 2·10·5
RB = 100/10 = 10 kN
ΣFy = 0: RA = 20 − 10 = 10 kN
w = 2 kN/mABRA​ = 10RB​ = 10section9 m1 m

Cut at x = 9 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 = 10·9 − 2·9·4.5 = 9 kN·m

Answer

Mx = 9 kN·m
10.Shear force & bending moment

Answer: MB = −20 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 = 10·10 = 100 kN, acting at x̄ = 5 m
ΣMA = 0: RB·8 = 10·10·5
RB = 500/8 = 62.5 kN
ΣFy = 0: RA = 100 − 62.5 = 37.5 kN

Cut at B and keep the overhang

The load on the overhang, w·a, acts at a/2 from B and makes the beam hog over the support.

MB = −w·a²/2 = −10·2²/2 = −20 kN·m

Answer

MB = −20 kN·m
11.Centroid & second moment of area

Answer: Ix = 16.99 × 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 = 300·20 = 6000 mm², yf = 140 + 20/2 = 150 mm
web: Aw = 20·140 = 2800 mm², yw = 140/2 = 70 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (6000·150 + 2800·70)/8800 = 124.5 mm

Parallel-axis theorem

flange: 300·20³/12 + 6000·(150 − 124.5)² = 4.088 × 10⁶ mm⁴
web: 20·140³/12 + 2800·(70 − 124.5)² = 1.29 × 10⁷ mm⁴
Ix = 4.088 × 10⁶ + 1.29 × 10⁷ = 1.699 × 10⁷ mm⁴ = 16.99 × 10⁶ mm⁴

Answer

Ix = 16.99 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σbottom = 149.7 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 = 100·15 = 1500 mm², yf = 180 + 15/2 = 187.5 mm
web: Aw = 20·180 = 3600 mm², yw = 180/2 = 90 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (1500·187.5 + 3600·90)/5100 = 118.7 mm

Parallel-axis theorem

flange: 100·15³/12 + 1500·(187.5 − 118.7)² = 7.133 × 10⁶ mm⁴
web: 20·180³/12 + 3600·(90 − 118.7)² = 1.268 × 10⁷ mm⁴
Ix = 7.133 × 10⁶ + 1.268 × 10⁷ = 1.981 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 118.7 mm
σ = M·y/I = 2.5 × 10⁷·118.7/1.981 × 10⁷ = 149.7 MPa

Answer

σbottom = 149.7 MPa

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