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
xyzdFAB

A constant force F = (−30, 0, −15) N acts on an object while it moves in a straight line from point A(−4, 0, 4) to point B(3, −1, −3). Coordinates are in metres. Find the work W done by the force.

F = (−30, 0, −15) NA(−4, 0, 4) mB(3, −1, −3) m
W = J
2.Vectors: dot & cross productHard
xyzab

Find the area A of the parallelogram spanned by a = (−6, 1, −5) and b = (2, −1, 0).

a = (−6, 1, −5)b = (2, −1, 0)
A =
3.Beam support reactionsMedium
P = 60 kNM = 30 kN·mABRB​ = ?5 m1 m2 m

The simply supported beam has a pin at A and a roller at B. It carries a point load P at 5 m from A and a counter-clockwise couple M at 6 m from A. Find the vertical reaction RB, taking upward as positive.

L = 8 mP = 60 kN at 5 mM = 30 kN·m (counter-clockwise) at 6 m
RB = kN
4.Beam support reactionsHard
w = 10 kN/mP = 10 kNABRA​ = ?RB​3 m0.5 m2.5 m

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

L = 6 mP = 10 kN at 3.5 mw = 10 kN/m from 3 to 6 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB60 kN8 m1 m4 m

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

span = 8 mheight = 4 mB is 1 m from Avertical load = 60 kN
FBC = kN
6.Truss: method of jointsHard
ABBCACACB50 kN15 kN5 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 = 5 mheight = 2 mB is 3 m from Avertical load = 50 kNhorizontal load = 15 kN ←
FAB = kN
7.Frames & machinesMedium
3 kN1.5 m0.9 m1.5 mABCD

A horizontal beam AB is pinned to a wall at A and propped by the strut CD, pinned to the wall at C, 1.5 m below A. A load of 3 kN hangs at B. Neglect the weights. Find the magnitude of the pin force A on the beam at A.

P = 3 kNAD = 1.5 mAB = 2.4 mAC = 1.5 m
A = kN
8.Frames & machinesHard
10 kN3 m1.2 m2.4 m0.75 mABCDEK

The A-frame shown stands on a pin at A and a roller at B, 3 m apart, with its apex pin C 3.6 m high and the horizontal tie DE 1.2 m above the ground. A vertical load of 10 kN acts on leg AC at K, 0.75 m (horizontally) from A. Find the magnitude of the force C that the pin C exerts on leg BC.

P = 10 kNAB = 3 mheight of C = 3.6 mheight of DE = 1.2 mhorizontal distance A to K = 0.75 m
C = kN
9.Shear force & bending momentMedium
4 kN/m60 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.

60 kN @ 8 m4 kN/m, 0–12 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)
10.Shear force & bending momentHard
w = 8 kN/mP = 60 kNABsection2 m4 m2 m

Find the bending moment Mx at the section x = 6 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 60 kN at 2 mw = 8 kN/m from 0 to 8 mx = 6 m
Mx = kN·m
11.Centroid & second moment of areaMedium
150 mm200 mm130 mmØ60xIx​ = ?

A 150 mm × 200 mm plate has a circular hole of diameter 60 mm on its vertical centre line, with its centre 130 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 150 mmh = 200 mmd = 60 mmhole centre: y = 130 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2802524012xM = 10 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 10 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 280 mmtf = 25 mmtw = 12 mmhw = 240 mmM = 10 kN·m
σtop = MPa

3Solutions

1.Vectors: dot & cross product

Answer: W = −105 J

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.

Displacement

d = B − A = (3, −1, −3) − (−4, 0, 4) = (7, −1, −7) m

Work

W = F·d = (−30)·7 + 0·(−1) + (−15)·(−7) = −105 J

Answer

W = −105 J

Negative work: the force acts mostly against the motion.

2.Vectors: dot & cross product

Answer: A = 11.87

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 = 1·0 − (−5)·(−1) = −5
(a × b)y = azbx − axbz = (−5)·2 − (−6)·0 = −10
(a × b)z = axby − aybx = (−6)·(−1) − 1·2 = 4

Area

A = |a × b| = √((−5)² + (−10)² + 4²) = 11.87

Answer

A = 11.87
3.Beam support reactions

Answer: RB = 33.75 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·8 − 60·5 + 30 = 0
RB = 270/8 = 33.75 kN

Vertical equilibrium

RA = 60 − 33.75 = 26.25 kN

Answer

RB = 33.75 kN

A negative reaction acts downward.

4.Beam support reactions

Answer: RA = 11.67 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 = 10 kNABRA​RB​3 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 = 10·3 = 30 kN, acting at x̄ = 4.5 m
ΣMA = 0: RB·6 = 10·3.5 + 10·3·4.5
RB = 170/6 = 28.33 kN
ΣFy = 0: RA = 40 − 28.33 = 11.67 kN

Answer

RA = 11.67 kN
5.Truss: method of joints

Answer: FBC = −15.12 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.

ABBCACACB60 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 60·1 → Cy = 7.5 kN
ΣFy = 0: Ay = 60 − 7.5 = 52.5 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 = 4/8.062 = 0.4961, cos γ = 7/8.062 = 0.8682
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −7.5/0.4961 = −15.12 kN

Answer

FBC = −15.12 kN (compression)
6.Truss: method of joints

Answer: FAB = −46.87 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 kN15 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 50·3 − 15·2 → Cy = 24 kN
ΣFy = 0: Ay = 50 − 24 = 26 kN
ΣFx = 0: Ax = 15 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 = −26/0.5547 = −46.87 kN

Answer

FAB = −46.87 kN (compression)
7.Frames & machines

Answer: A = 5.126 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.

Strut force

FCD = 3·2.4/(0.7071·1.5) = 6.788 kN

Components at A

Ax = FCD·cos α = 4.8 kN (towards the wall)
Ay = 3 − FCD·sin α = −1.8 kN

Magnitude

A = √(4.8² + −1.8²) = 5.126 kN

Answer

A = 5.126 kN

A negative Ay means the wall pulls the beam down at A.

8.Frames & machines

Answer: C = 2.948 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 = 10·0.75/3 = 2.5 kN

Tie force

T = 2.5·1.5/2.4 = 1.562 kN

Pin force on BC

Cx = 1.562 kN, Cy = −2.5 kN
C = √(1.562² + 2.5²) = 2.948 kN

Answer

C = 2.948 kN
9.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 = 44 kN, R2 = 64 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 = 80, MC = 144, MD = 192, ME = 224 kN·m, MF = 120, MG = 0

Answer

Mark E: ME = 224 kN·m
10.Shear force & bending moment

Answer: Mx = 78 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 = 8·8 = 64 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 60·2 + 8·8·4
RB = 376/8 = 47 kN
ΣFy = 0: RA = 124 − 47 = 77 kN
w = 8 kN/mP = 60 kNABRA​ = 77RB​ = 47section2 m4 m2 m

Cut at x = 6 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 = 77·6 − 60·(6 − 2) − 8·6·3 = 78 kN·m

Answer

Mx = 78 kN·m
11.Centroid & second moment of area

Answer: Ix = 96.55 × 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 = (30000·100 − 2827·130)/(30000 − 2827) = 96.88 mm

Full plate about ȳ

150·200³/12 + 30000·3.122² = 100.3 × 10⁶ mm⁴

Hole about ȳ

π·60⁴/64 + 2827·33.12² = 3.738 × 10⁶ mm⁴

Subtract

Ix = 96.55 × 10⁶ mm⁴

Answer

Ix = 96.55 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 10.22 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 = 280·25 = 7000 mm², yf = 240 + 25/2 = 252.5 mm
web: Aw = 12·240 = 2880 mm², yw = 240/2 = 120 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (7000·252.5 + 2880·120)/9880 = 213.9 mm

Parallel-axis theorem

flange: 280·25³/12 + 7000·(252.5 − 213.9)² = 1.081 × 10⁷ mm⁴
web: 12·240³/12 + 2880·(120 − 213.9)² = 3.92 × 10⁷ mm⁴
Ix = 1.081 × 10⁷ + 3.92 × 10⁷ = 5.001 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 265 − 213.9 = 51.12 mm
σ = M·y/I = 1 × 10⁷·51.12/5.001 × 10⁷ = 10.22 MPa

Answer

σtop = 10.22 MPa

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