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 = (−2, 3, 2) onto b = (1, −3, 2), that is, the component of a in the direction of b.

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

For a = (−5, 3, −3) and b = (4, −4, 5), find the z-component (a × b)z of the cross product a × b.

a = (−5, 3, −3)b = (4, −4, 5)
(a × b)z =
3.Beam support reactionsMedium
P1​ = 40 kNP2​ = 15 kNABRA​ = ?RB​1.5 m2 m1.5 m

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

L = 5 mP1 = 40 kN at 1.5 mP2 = 15 kN at 3.5 m
RA = kN
4.Beam support reactionsHard
w = 8 kN/mP = 25 kNABRA​RB​ = ?3 m0.5 m1.5 m

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

L = 5 mP = 25 kN at 3.5 mw = 8 kN/m from 3 to 5 m
RB = kN
5.Truss: method of jointsMedium
ABBCACACB55 kN5 m2 m4 m

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

span = 5 mheight = 4 mB is 2 m from Avertical load = 55 kN
FAC = kN
6.Truss: method of jointsHard
ABBCACACB10 kN25 kN8 m7 m3 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 = 3 mB is 7 m from Avertical load = 10 kNhorizontal load = 25 kN →
FAB = kN
7.Frames & machinesMedium
8 kN6 m0.8 m1.7 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, 2.5 m high, and the horizontal tie DE is 0.8 m above the ground. A load of 8 kN acts at C. Find the magnitude of the force C that the pin C exerts on leg BC.

P = 8 kNAB = 6 mheight of C = 2.5 mheight of DE = 0.8 m
C = kN
8.Frames & machinesHard
w = 3 kN/m2 kN0.8 m0.7 m0.75 mABCD

The beam AB of the wall bracket shown is pinned at A and propped by the strut CD (C is 0.75 m below A). The beam carries a uniform load of 3 kN/m over its full length and a point load of 2 kN at its free end B. Find the force FCD in the strut.

w = 3 kN/mP = 2 kNAD = 0.8 mAB = 1.5 mAC = 0.75 m
FCD = kN
9.Shear force & bending momentMedium
8 kN/m20 kNABCDEFG1 m1 m1 m1 m1 m1 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.

20 kN @ 2 m8 kN/m, 1–4 m
  1. 1A (x = 0 m)
  2. 2B (x = 1 m)
  3. 3C (x = 2 m)
  4. 4D (x = 3 m)
  5. 5E (x = 4 m)
  6. 6F (x = 5 m)
  7. 7G (x = 6 m)
10.Shear force & bending momentHard
6 kN/m45 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.

45 kN @ 12 m6 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
160150t = 20xdimensions in mm

A channel section lies with its open side up: a base plate 160 mm wide with two upright legs, 150 mm high overall. Base and legs are all 20 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.

b = 160 mmh = 150 mmt = 20 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
140302608xM = 5 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 5 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 140 mmtf = 30 mmtw = 8 mmhw = 260 mmM = 5 kN·m
σbottom = MPa

3Solutions

1.Vectors: dot & cross product

Answer: compb a = −1.871

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 = (−2)·1 + 3·(−3) + 2·2 = −7

Length of b

|b| = √(1² + (−3)² + 2²) = 3.742

Scalar projection

compb a = a·b/|b| = −7/3.742 = −1.871

Answer

compb a = −1.871

Negative: a has a component pointing against b.

2.Vectors: dot & cross product

Answer: (a × b)z = 8

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 = 3·5 − (−3)·(−4) = 3
(a × b)y = azbx − axbz = (−3)·4 − (−5)·5 = 13
(a × b)z = axby − aybx = (−5)·(−4) − 3·4 = 8

Requested component

(a × b)z = 8

Answer

(a × b)z = 8

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

3.Beam support reactions

Answer: RA = 32.5 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.

P1​ = 40 kNP2​ = 15 kNABRA​RB​1.5 m2 m1.5 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.

ΣMA = 0: RB·5 = 40·1.5 + 15·3.5
RB = 112.5/5 = 22.5 kN
ΣFy = 0: RA = 55 − 22.5 = 32.5 kN

Answer

RA = 32.5 kN
4.Beam support reactions

Answer: RB = 30.3 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 = 8 kN/mP = 25 kNABRA​RB​3 m0.5 m1.5 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 = 8·2 = 16 kN, acting at x̄ = 4 m
ΣMA = 0: RB·5 = 25·3.5 + 8·2·4
RB = 151.5/5 = 30.3 kN
ΣFy = 0: RA = 41 − 30.3 = 10.7 kN

Answer

RB = 30.3 kN
5.Truss: method of joints

Answer: FAC = 16.5 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.

ABBCACACB55 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 55·2 → Cy = 22 kN
ΣFy = 0: Ay = 55 − 22 = 33 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 = 4/5 = 0.8, cos γ = 3/5 = 0.6
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −22/0.8 = −27.5 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−27.5)·0.6 = 16.5 kN

Answer

FAC = 16.5 kN (tension)
6.Truss: method of joints

Answer: FAB = 20.63 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 kN25 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 10·7 + 25·3 → Cy = 18.13 kN
ΣFy = 0: Ay = 10 − 18.13 = −8.125 kN
ΣFx = 0: Ax = −25 kN

Joint A

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

sin α = 3/7.616 = 0.3939
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −−8.125/0.3939 = 20.63 kN

Answer

FAB = 20.63 kN (tension)
7.Frames & machines

Answer: C = 8.113 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 = 4 kN
T = 4·3/1.7 = 7.059 kN

Components of the pin force on BC

Cx = T = 7.059 kN, Cy = −By = −4 kN

Magnitude

C = √(7.059² + 4²) = 8.113 kN

Answer

C = 8.113 kN
8.Frames & machines

Answer: FCD = 11.65 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 = 3·1.5 = 4.5 kN at 0.75 m

Moments about A for the beam

FCD·0.6839·0.8 = 4.5·0.75 + 2·1.5 = 6.375 kN·m
FCD = 11.65 kN

Answer

FCD = 11.65 kN
9.Shear force & bending moment

Answer: C (x = 2 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 = 27.33 kN, R2 = 16.67 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 = 27.33, MC = 50.67 kN·m, MD = 46, ME = 33.33, MF = 16.67, MG = 0

Answer

Mark C: MC = 50.67 kN·m
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 = 1.5 kN, R2 = 91.5 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 = −9, MC = −42, MD = −99, ME = −180 kN·m, MF = −90, MG = 0

Answer

Mark E: ME = −180 kN·m
11.Centroid & second moment of area

Answer: Ix = 18.57 × 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 = 160·20 = 3200 mm², y1 = 10 mm
two legs: A2 = 2·20·130 = 5200 mm², y2 = 20 + 130/2 = 85 mm

Centroid

ȳ = (3200·10 + 5200·85)/8400 = 56.43 mm

Parallel-axis theorem

base: 160·20³/12 + 3200·(10 − 56.43)² = 7.005 × 10⁶ mm⁴
two legs: 2·20·130³/12 + 5200·(85 − 56.43)² = 1.157 × 10⁷ mm⁴
Ix = 7.005 × 10⁶ + 1.157 × 10⁷
Ix = 1.857 × 10⁷ mm⁴ = 18.57 × 10⁶ mm⁴

Answer

Ix = 18.57 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σbottom = 27.49 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 = 140·30 = 4200 mm², yf = 260 + 30/2 = 275 mm
web: Aw = 8·260 = 2080 mm², yw = 260/2 = 130 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4200·275 + 2080·130)/6280 = 227 mm

Parallel-axis theorem

flange: 140·30³/12 + 4200·(275 − 227)² = 1 × 10⁷ mm⁴
web: 8·260³/12 + 2080·(130 − 227)² = 3.128 × 10⁷ mm⁴
Ix = 1 × 10⁷ + 3.128 × 10⁷ = 4.128 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 227 mm
σ = M·y/I = 5 × 10⁶·227/4.128 × 10⁷ = 27.49 MPa

Answer

σbottom = 27.49 MPa

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