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 = (1, 0, −6) and b = (−1, 4, 0), in degrees.

a = (1, 0, −6)b = (−1, 4, 0)
θ = °
2.Vectors: dot & cross productHard
xyzab

The unit vector n̂ is perpendicular to both a = (−3, 4, −2) and b = (−2, −1, −3) and has a positive z-component. Find its y-component n̂y.

a = (−3, 4, −2)b = (−2, −1, −3)n̂z > 0
n̂y =
3.Beam support reactionsMedium
w0​ = 15 kN/mP = 45 kNABRA​ = ?4.5 m1.5 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that rises from zero at A to 15 kN/m at B. A point load P also acts at 4.5 m from A. Find the vertical support reaction RA.

L = 6 mw0 = 15 kN/mP = 45 kN at 4.5 m
RA = kN
4.Beam support reactionsHard
w = 2 kN/mP = 50 kNABRA​ = ?RB​2 m4 m1 m1 m

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

L = 8 mP = 50 kN at 2 mw = 2 kN/m from 6 to 7 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB30 kN8 m3 m2 m

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

span = 8 mheight = 2 mB is 3 m from Avertical load = 30 kN
FAB = kN
6.Truss: method of jointsHard
ABBCACACB40 kN5 kN6 m5 m4 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 = 4 mB is 5 m from Avertical load = 40 kNhorizontal load = 5 kN →
FAC = kN
7.Frames & machinesMedium
150 NQ = ?30°ABC

In the toggle clamp shown, two equal links AB and BC are pinned together at B, and each makes 30° with the line AC. A downward force of 150 N is applied at B. The slider C presses on a workpiece. Neglecting friction and weights, find the horizontal clamping force Q.

F = 150 Nθ = 30°
Q = N
8.Frames & machinesHard
20 kN4 m1.5 m1.5 m1.5 mABCDEK

The A-frame shown stands on a pin at A and a roller at B, 4 m apart, with its apex pin C 3 m high and the horizontal tie DE 1.5 m above the ground. A vertical load of 20 kN acts on leg AC at K, 1.5 m (horizontally) from A. Find the magnitude of the force C that the pin C exerts on leg BC.

P = 20 kNAB = 4 mheight of C = 3 mheight of DE = 1.5 mhorizontal distance A to K = 1.5 m
C = kN
9.Shear force & bending momentMedium
w = 6 kN/mABsection2 m2 m

Find the bending moment Mx at the section x = 2 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mw = 6 kN/m from 0 to 4 mx = 2 m
Mx = kN·m
10.Shear force & bending momentHard
w = 4 kN/mP = 20 kNABsection1 m3 m

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

L = 4 mP = 20 kN at 1 mw = 4 kN/m from 0 to 4 mx = 1 m
Mx = kN·m
11.Centroid & second moment of areaMedium
2203030018xdimensions in mm

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

bf = 220 mmtf = 30 mmtw = 18 mmhw = 300 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
190160222501216xdimensions in mm

A welded I-section has a top flange 190 × 22 mm, a web 250 mm high and 16 mm thick, and a bottom flange 160 × 12 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 190 × 22 mmweb: 16 × 250 mmbottom flange: 160 × 12 mm
Ix = × 10⁶ mm⁴

3Solutions

1.Vectors: dot & cross product

Answer: θ = 92.29 °

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 = 1·(−1) + 0·4 + (−6)·0 = −1

Magnitudes

|a| = √(1² + 0² + (−6)²) = 6.083
|b| = √((−1)² + 4² + 0²) = 4.123

Angle

cos θ = −1/(6.083·4.123) = −0.03987
θ = arccos(−0.03987) = 92.29°

Answer

θ = 92.29°
2.Vectors: dot & cross product

Answer: n̂y = −0.2704

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·(−3) − (−2)·(−1) = −14
(a × b)y = azbx − axbz = (−2)·(−2) − (−3)·(−3) = −5
(a × b)z = axby − aybx = (−3)·(−1) − 4·(−2) = 11

Normalise

The z-component of a × b is already positive.

|a × b| = √((−14)² + (−5)² + 11²) = 18.49
n̂ = (−14, −5, 11)/18.49 = (−0.757, −0.2704, 0.5948)
n̂y = −0.2704

Answer

n̂y = −0.2704
3.Beam support reactions

Answer: RA = 26.25 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 = ½·15·6 = 45 kN
x̄ = 2L/3 = 4 m

Equilibrium

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

ΣMA = 0: RB·6 = 45·4 + 45·4.5
RB = 63.75 kN
RA = 90 − 63.75 = 26.25 kN

Answer

RA = 26.25 kN
4.Beam support reactions

Answer: RA = 37.88 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 = 2 kN/mP = 50 kNABRA​RB​2 m4 m1 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 = 2·1 = 2 kN, acting at x̄ = 6.5 m
ΣMA = 0: RB·8 = 50·2 + 2·1·6.5
RB = 113/8 = 14.13 kN
ΣFy = 0: RA = 52 − 14.13 = 37.88 kN

Answer

RA = 37.88 kN
5.Truss: method of joints

Answer: FAB = −33.8 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 30·3 → Cy = 11.25 kN
ΣFy = 0: Ay = 30 − 11.25 = 18.75 kN

Joint A

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

sin α = 2/3.606 = 0.5547
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −18.75/0.5547 = −33.8 kN

Answer

FAB = −33.8 kN (compression)
6.Truss: method of joints

Answer: FAC = 9.167 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.

ABBCACACB40 kN5 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 40·5 + 5·4 → Cy = 36.67 kN
ΣFy = 0: Ay = 40 − 36.67 = 3.333 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 = 4/4.123 = 0.9701, cos γ = 1/4.123 = 0.2425
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −36.67/0.9701 = −37.8 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−37.8)·0.2425 = 9.167 kN

Answer

FAC = 9.167 kN (tension)
7.Frames & machines

Answer: Q = 129.9 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 30° = 150
Flink = 150 N

Clamping force

Q = Flink·cos 30° = 150/(2·tan 30°) = 129.9 N

Answer

Q = 129.9 N

The force ratio Q/F = 0.866 grows without limit as the links straighten.

8.Frames & machines

Answer: C = 12.5 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.

Support reaction at B

By = 20·1.5/4 = 7.5 kN

Tie force

T = 7.5·2/1.5 = 10 kN

Pin force on BC

Cx = 10 kN, Cy = −7.5 kN
C = √(10² + 7.5²) = 12.5 kN

Answer

C = 12.5 kN
9.Shear force & bending moment

Answer: Mx = 12 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 = 6·4 = 24 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 6·4·2
RB = 48/4 = 12 kN
ΣFy = 0: RA = 24 − 12 = 12 kN
w = 6 kN/mABRA​ = 12RB​ = 12section2 m2 m

Cut at x = 2 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 = 12·2 − 6·2·1 = 12 kN·m

Answer

Mx = 12 kN·m
10.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 = 4·4 = 16 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 20·1 + 4·4·2
RB = 52/4 = 13 kN
ΣFy = 0: RA = 36 − 13 = 23 kN
w = 4 kN/mP = 20 kNABRA​ = 23RB​ = 13section1 m3 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.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 23·1 − 4·1·0.5 = 21 kN·m

Answer

Mx = 21 kN·m
11.Centroid & second moment of area

Answer: Ix = 121.9 × 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 = 220·30 = 6600 mm², yf = 300 + 30/2 = 315 mm
web: Aw = 18·300 = 5400 mm², yw = 300/2 = 150 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (6600·315 + 5400·150)/12000 = 240.8 mm

Parallel-axis theorem

flange: 220·30³/12 + 6600·(315 − 240.8)² = 3.688 × 10⁷ mm⁴
web: 18·300³/12 + 5400·(150 − 240.8)² = 8.497 × 10⁷ mm⁴
Ix = 3.688 × 10⁷ + 8.497 × 10⁷ = 1.219 × 10⁸ mm⁴ = 121.9 × 10⁶ mm⁴

Answer

Ix = 121.9 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 121.3 × 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 three rectangles

Measure every y from the bottom edge.

top flange: A = 4180 mm², y = 273 mm
web: A = 4000 mm², y = 137 mm
bottom flange: A = 1920 mm², y = 6 mm

Centroid

ȳ = (4180·273 + 4000·137 + 1920·6)/10100 = 168.4 mm

Parallel-axis theorem

top flange: 190·22³/12 + 4180·104.6² = 4.592 × 10⁷ mm⁴
web: 16·250³/12 + 4000·31.38² = 2.477 × 10⁷ mm⁴
bottom flange: 160·12³/12 + 1920·162.4² = 5.065 × 10⁷ mm⁴
Ix = 4.592 × 10⁷ + 2.477 × 10⁷ + 5.065 × 10⁷
Ix = 1.213 × 10⁸ mm⁴ = 121.3 × 10⁶ mm⁴

Answer

Ix = 121.3 × 10⁶ mm⁴

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