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, −1) and b = (−5, 4, 3), in degrees.

a = (1, 0, −1)b = (−5, 4, 3)
θ = °
2.Vectors: dot & cross productHard
xyzrFOA

A force F = (−60, 40, −20) N acts at point A(−2, −3, 2). Coordinates are in metres. Find the x-component Mx of the moment of the force about point O(−2, 1, −2).

F = (−60, 40, −20) NA(−2, −3, 2) mO(−2, 1, −2) m
Mx = N·m
3.Beam support reactionsMedium
P1​ = 10 kNP2​ = 20 kNABRA​RB​ = ?3 m2 m1 m

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

L = 6 mP1 = 10 kN at 3 mP2 = 20 kN at 5 m
RB = kN
4.Beam support reactionsHard
w0​ = 6 kN/mP = 50 kNABMA​ = ?10 m

The cantilever beam is fixed to the wall at A. It carries a linearly varying load that is zero at the wall and rises to 6 kN/m at the free end B, plus a point load P at 10 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 10 mw0 = 6 kN/mP = 50 kN at 10 m
MA = kN·m
5.Truss: method of jointsMedium
ABBCACACB10 kN8 m1 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 1 m from Avertical load = 10 kN
FAB = kN
6.Truss: method of jointsHard
ABBCACACB15 kN10 kN6 m4 m2 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 = 2 mB is 4 m from Avertical load = 15 kNhorizontal load = 10 kN →
FAB = kN
7.Frames & machinesMedium
6 kN6 m2 m2.7 mABCK

The frame shown has pins at A, B and C; A and C are fixed to the ground 6 m apart, and B is 2 m above the ground and 2.7 m to the right of A. A vertical load of 6 kN acts on member AB at K, 2.025 m (horizontally) from A. Find the force FBC in member BC.

P = 6 kNL = 6 mH = 2 mhorizontal distance A to B = 2.7 mhorizontal distance A to K = 2.025 m
FBC = kN
8.Frames & machinesHard
F = ?3000 N12 mmABC

A toggle press has two equal links AB and BC, each 200 mm long between pins. The joint B sits 12 mm above the line AC. Which downward force F at B produces a horizontal pressing force of 3000 N at the slider C? Neglect friction and weights.

Q = 3000 NAB = BC = 200 mmh = 12 mm
F = N
9.Shear force & bending momentMedium
w = 5 kN/mABsection3.5 m1.5 m

Find the bending moment Mx at the section x = 3.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mw = 5 kN/m from 0 to 5 mx = 3.5 m
Mx = kN·m
10.Shear force & bending momentHard
w = 8 kN/mABC5 m2.5 m

The beam rests on a pin at A and a roller at B and overhangs B by 2.5 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 = 7.5 mw = 8 kN/m from 0 to 7.5 msupports at x = 0 and x = 5 m
MB = kN·m
11.Centroid & second moment of areaMedium
110460108xdimensions in mm

A symmetric I-section has flanges 110 mm wide and 10 mm thick, an overall depth of 460 mm and a web 8 mm thick. Find its second moment of area Ix about the horizontal centroidal axis x.

B = 110 mmH = 460 mmtf = 10 mmtw = 8 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2201026010xM = 15 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 15 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 220 mmtf = 10 mmtw = 10 mmhw = 260 mmM = 15 kN·m
σtop = MPa

3Solutions

1.Vectors: dot & cross product

Answer: θ = 143.1 °

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·(−5) + 0·4 + (−1)·3 = −8

Magnitudes

|a| = √(1² + 0² + (−1)²) = 1.414
|b| = √((−5)² + 4² + 3²) = 7.071

Angle

cos θ = −8/(1.414·7.071) = −0.8
θ = arccos(−0.8) = 143.1°

Answer

θ = 143.1°
2.Vectors: dot & cross product

Answer: Mx = −80 N·m

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.

Position vector from O to A

r = A − O = (−2, −3, 2) − (−2, 1, −2) = (0, −4, 4) m

Moment M = r × F

(r × F)x = ryFz − rzFy = (−4)·(−20) − 4·40 = −80 N·m
(r × F)y = rzFx − rxFz = 4·(−60) − 0·(−20) = −240 N·m
(r × F)z = rxFy − ryFx = 0·40 − (−4)·(−60) = −240 N·m

Requested component

Mx = −80 N·m

Answer

Mx = −80 N·m
3.Beam support reactions

Answer: RB = 21.67 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.

P1​ = 10 kNP2​ = 20 kNABRA​RB​3 m2 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.

ΣMA = 0: RB·6 = 10·3 + 20·5
RB = 130/6 = 21.67 kN
ΣFy = 0: RA = 30 − 21.67 = 8.333 kN

Answer

RB = 21.67 kN
4.Beam support reactions

Answer: MA = 700 kN·m

Cantilever equilibrium: a fixed support can push up and also resist rotation, so it gives a vertical reaction RA and a reaction moment MA. ΣFy = 0 gives RA, and moments about the wall give MA = Σ(load × distance from the wall). A distributed load acts as its resultant at the centroid of the load diagram.

Resultant of the triangular load

W = ½·6·10 = 30 kN
x̄ = 2L/3 = 6.667 m

Moment about the wall

MA = W·x̄ + P·a = 30·6.667 + 50·10 = 700 kN·m

Answer

MA = 700 kN·m
5.Truss: method of joints

Answer: FAB = −9.783 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 10·1 → Cy = 1.25 kN
ΣFy = 0: Ay = 10 − 1.25 = 8.75 kN

Joint A

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

sin α = 2/2.236 = 0.8944
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −8.75/0.8944 = −9.783 kN

Answer

FAB = −9.783 kN (compression)
6.Truss: method of joints

Answer: FAB = −3.727 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.

ABBCACACB15 kN10 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 15·4 + 10·2 → Cy = 13.33 kN
ΣFy = 0: Ay = 15 − 13.33 = 1.667 kN
ΣFx = 0: Ax = −10 kN

Joint A

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

sin α = 2/4.472 = 0.4472
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −1.667/0.4472 = −3.727 kN

Answer

FAB = −3.727 kN (compression)
7.Frames & machines

Answer: FBC = 3.907 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 = √(3.3² + 2²) = 3.859 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·(2/3.859)·6 = 6·2.025
FBC = 3.907 kN (compression)

Answer

FBC = 3.907 kN
8.Frames & machines

Answer: F = 360.6 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 = 12/200 = 0.06, θ = 3.44°

Link force

Flink = Q/cos θ = 3005 N

Force at B

F = 2·Flink·sin θ = 2·3000·tan θ = 360.6 N

Answer

F = 360.6 N
9.Shear force & bending moment

Answer: Mx = 13.13 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 = 5·5 = 25 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 5·5·2.5
RB = 62.5/5 = 12.5 kN
ΣFy = 0: RA = 25 − 12.5 = 12.5 kN
w = 5 kN/mABRA​ = 12.5RB​ = 12.5section3.5 m1.5 m

Cut at x = 3.5 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 = 12.5·3.5 − 5·3.5·1.75 = 13.13 kN·m

Answer

Mx = 13.13 kN·m
10.Shear force & bending moment

Answer: MB = −25 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 = 8·7.5 = 60 kN, acting at x̄ = 3.75 m
ΣMA = 0: RB·5 = 8·7.5·3.75
RB = 225/5 = 45 kN
ΣFy = 0: RA = 60 − 45 = 15 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 = −8·2.5²/2 = −25 kN·m

Answer

MB = −25 kN·m
11.Centroid & second moment of area

Answer: Ix = 168.2 × 10⁶ mm⁴

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.

Outer rectangle minus the two side cut-outs

Both cut-outs together are (B − tw) wide and hw = H − 2tf high, and share the axis x.

hw = 460 − 2·10 = 440 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (110·460³ − 102·440³)/12
Ix = 1.682 × 10⁸ mm⁴ = 168.2 × 10⁶ mm⁴

Answer

Ix = 168.2 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 32.21 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 = 220·10 = 2200 mm², yf = 260 + 10/2 = 265 mm
web: Aw = 10·260 = 2600 mm², yw = 260/2 = 130 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2200·265 + 2600·130)/4800 = 191.9 mm

Parallel-axis theorem

flange: 220·10³/12 + 2200·(265 − 191.9)² = 1.178 × 10⁷ mm⁴
web: 10·260³/12 + 2600·(130 − 191.9)² = 2.46 × 10⁷ mm⁴
Ix = 1.178 × 10⁷ + 2.46 × 10⁷ = 3.638 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 270 − 191.9 = 78.13 mm
σ = M·y/I = 1.5 × 10⁷·78.13/3.638 × 10⁷ = 32.21 MPa

Answer

σtop = 32.21 MPa

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