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 = (2, 0, −5) and b = (0, −6, 5), in degrees.

a = (2, 0, −5)b = (0, −6, 5)
θ = °
2.Vectors: dot & cross productHard
xyzabc

Find the volume V of the parallelepiped whose edges from one corner are a = (−1, 0, −3), b = (−4, 2, −1) and c = (−4, −1, −4).

a = (−1, 0, −3)b = (−4, 2, −1)c = (−4, −1, −4)
V =
3.Beam support reactionsMedium
P = 35 kNM = 20 kN·mABRA​ = ?4 m0.5 m0.5 m

The simply supported beam has a pin at A and a roller at B. It carries a point load P at 4.5 m from A and a counter-clockwise couple M at 4 m from A. Find the vertical reaction RA, taking upward as positive.

L = 5 mP = 35 kN at 4.5 mM = 20 kN·m (counter-clockwise) at 4 m
RA = kN
4.Beam support reactionsHard
P = 40 kNQ = 65 kNADCMA​ = ?1 m3 m2 m4 m

A compound beam is fixed to the wall at A, has an internal hinge at C (4 m from A) and rests on a roller at D (10 m from A). It carries a point load P at 6 m from A and a point load Q at 1 m from A. Find the magnitude of the reaction moment MA at the wall.

AC = 4 mAD = 10 mP = 40 kN at 6 mQ = 65 kN at 1 m
MA = kN·m
5.Truss: method of jointsMedium
ABBCACACB35 kN5 m2 m3 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 = 3 mB is 2 m from Avertical load = 35 kN
FAB = kN
6.Truss: method of jointsHard
ABCDEFGH10 kN35 kN25 kN35 kN4 × 3 m3 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

B: 10 kN ↓D: 35 kN ↓F: 25 kN ↓F: 35 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 FC
  13. 13member HC
7.Frames & machinesMedium
5 kN5 m2 m0.75 mABCK

The frame shown has pins at A, B and C; A and C are fixed to the ground 5 m apart, and B is 2 m above the ground and 0.75 m to the right of A. A vertical load of 5 kN acts on member AB at K, 0.375 m (horizontally) from A. Find the force FBC in member BC.

P = 5 kNL = 5 mH = 2 mhorizontal distance A to B = 0.75 mhorizontal distance A to K = 0.375 m
FBC = kN
8.Frames & machinesHard
8 kN0.5 kN2 m2.5 mABC

A uniform horizontal boom AB of weight 0.5 kN is pinned to a wall at A and held by a cable from its end B to the point C on the wall, 2.5 m above A. A load of 8 kN hangs at B. Find the tension T in the cable.

W = 8 kNWb = 0.5 kNAB = 2 mAC = 2.5 m
T = kN
9.Shear force & bending momentMedium
w = 3 kN/mABsection3 m3 m

Find the bending moment Mx at the section x = 3 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 6 mw = 3 kN/m from 0 to 6 mx = 3 m
Mx = kN·m
10.Shear force & bending momentHard
5 kN/m45 kN15 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 @ 0 m15 kN @ 12 m5 kN/m, 2–8 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
B = 220H = 225t = 16xdimensions in mm

A hollow rectangular (box) section has outer width B = 220 mm, outer height H = 225 mm and a uniform wall thickness t = 16 mm. Find its radius of gyration r about the horizontal centroidal axis.

B = 220 mmH = 225 mmt = 16 mm
r = mm
12.Centroid & second moment of areaHard
2602010016xhogging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 30 MPa in tension and 120 MPa in compression. Find the largest hogging bending moment Mallow the beam can carry (give its size).

bf = 260 mmtf = 20 mmtw = 16 mmhw = 100 mmσt,allow = 30 MPaσc,allow = 120 MPa
Mallow = kN·m

3Solutions

1.Vectors: dot & cross product

Answer: θ = 126.5 °

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 = 2·0 + 0·(−6) + (−5)·5 = −25

Magnitudes

|a| = √(2² + 0² + (−5)²) = 5.385
|b| = √(0² + (−6)² + 5²) = 7.81

Angle

cos θ = −25/(5.385·7.81) = −0.5944
θ = arccos(−0.5944) = 126.5°

Answer

θ = 126.5°
2.Vectors: dot & cross product

Answer: V = 27

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 = 2·(−4) − (−1)·(−1) = −9
(b × c)y = bzcx − bxcz = (−1)·(−4) − (−4)·(−4) = −12
(b × c)z = bxcy − bycx = (−4)·(−1) − 2·(−4) = 12

Dot product with a

a·(b × c) = (−1)·(−9) + 0·(−12) + (−3)·12 = −27
V = |−27| = 27

Answer

V = 27
3.Beam support reactions

Answer: RA = 7.5 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.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·5 − 35·4.5 + 20 = 0
RB = 137.5/5 = 27.5 kN

Vertical equilibrium

RA = 35 − 27.5 = 7.5 kN

Answer

RA = 7.5 kN

A negative reaction acts downward.

4.Beam support reactions

Answer: MA = 171.7 kN·m

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. An internal hinge cannot carry a bending moment, which gives one extra equation: the moment about the hinge of the forces on either side is zero.

Part CD

The hinge has no moment, so moments about C on CD alone must balance.

ΣMC = 0: RD·6 = 40·2
RD = 13.33 kN
VC = 40 − 13.33 = 26.67 kN

Part AC

The hinge force VC acts downward on AC (equal and opposite to its action on CD).

RA = 65 + 26.67 = 91.67 kN
MA = 65·1 + 26.67·4 = 171.7 kN·m

Answer

MA = 171.7 kN·m
5.Truss: method of joints

Answer: FAB = −25.24 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.

ABBCACACB35 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 35·2 → Cy = 14 kN
ΣFy = 0: Ay = 35 − 14 = 21 kN

Joint A

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

sin α = 3/3.606 = 0.8321
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −21/0.8321 = −25.24 kN

Answer

FAB = −25.24 kN (compression)
6.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 G

FG and GH 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: 61.25 kN (T), BC: 61.25 kN (T), CD: 43.75 kN (T), DE: 43.75 kN (T), FG: 52.5 kN (C), GH: 52.5 kN (C), AF: 37.12 kN (C), HE: 61.87 kN (C), BF: 10 kN (T), CG: 0, DH: 35 kN (T), FC: 12.37 kN (C), HC: 12.37 kN (T)

Answer

Zero-force member: CG
7.Frames & machines

Answer: FBC = 0.8807 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.

Two-force member BC

BC = √(4.25² + 2²) = 4.697 m

Whole frame: moments about A

The ground pushes on BC at C along CB; its horizontal component passes through A, only the vertical one has a moment.

FBC·(2/4.697)·5 = 5·0.375
FBC = 0.8807 kN (compression)

Answer

FBC = 0.8807 kN
8.Frames & machines

Answer: T = 10.57 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.

Cable angle

BC = √(2² + 2.5²) = 3.202 m, sin β = 0.7809

Moments about A

T·0.7809·2 = 8·2 + 0.5·1
T = 10.57 kN

Answer

T = 10.57 kN
9.Shear force & bending moment

Answer: Mx = 13.5 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 = 3·6 = 18 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 3·6·3
RB = 54/6 = 9 kN
ΣFy = 0: RA = 18 − 9 = 9 kN
w = 3 kN/mABRA​ = 9RB​ = 9section3 m3 m

Cut at x = 3 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 = 9·3 − 3·3·1.5 = 13.5 kN·m

Answer

Mx = 13.5 kN·m
10.Shear force & bending moment

Answer: B (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 = 65 kN, R2 = 25 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 = −90 kN·m, MC = −60, MD = −50, ME = −60, MF = −30, MG = 0

Answer

Mark B: MB = −90 kN·m
11.Centroid & second moment of area

Answer: r = 85.32 mm

Second moment of area: for a rectangle about its own centroidal axis I = bh³/12, and about its base bh³/3 (parallel-axis theorem I = Ic + A·d²). A hole is handled by subtracting its I, as long as both parts share the same axis. The elastic section modulus is S = I/c, where c is the distance to the extreme fibre. The radius of gyration r = √(I/A) is the distance at which the whole area would give the same I; it is used in column buckling.

Net area and second moment of area

b = 188 mm, h = 193 mm
A = BH − bh = 220·225 − 188·193 = 13216 mm²
I = (BH³ − bh³)/12 = 9.62 × 10⁷ mm⁴

Radius of gyration

r = √(I/A) = √(9.62 × 10⁷/13216) = 85.32 mm

Answer

r = 85.32 mm
12.Centroid & second moment of area

Answer: Mallow = 7.353 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 = (5200·110 + 1600·50)/6800 = 95.88 mm
top edge: c = 120 − 95.88 = 24.12 mm

Second moment of area

I = 260·20³/12 + 5200·14.12² + 16·100³/12 + 1600·45.88² = 5.911 × 10⁶ mm⁴

Moment allowed by each edge

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

top edge: M = 30·5.911 × 10⁶/24.12 = 7.353 kN·m
bottom edge: M = 120·5.911 × 10⁶/95.88 = 7.398 kN·m

Governing value

Mallow = min = 7.353 kN·m (top edge)

Answer

Mallow = 7.353 kN·m

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