Statics: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

New problemsBack to the course

In the print window, choose “Save as PDF” to keep a copy on your device.

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 dot product a·b of a = (−5, −7, 0) and b = (−6, 2, −1).

a = (−5, −7, 0)b = (−6, 2, −1)
a·b =
2.Vectors: dot & cross productHard
xyzABC

Find the area A of the triangle with corners A(−3, 1, −4), B(−2, −1, 1) and C(2, −4, 2). Coordinates are in metres.

A(−3, 1, −4)B(−2, −1, 1)C(2, −4, 2)
A = m²
3.Beam support reactionsMedium
P1​ = 10 kNP2​ = 40 kNABRA​ = ?RB​1 m4 m3 m

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

L = 8 mP1 = 10 kN at 1 mP2 = 40 kN at 5 m
RA = kN
4.Beam support reactionsHard
w = 5 kN/mP = 30 kNABRA​ = ?RB​2 m2 m6 m

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

L = 10 mP = 30 kN at 2 mw = 5 kN/m from 4 to 10 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB45 kN6 m4 m2 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 = 2 mB is 4 m from Avertical load = 45 kN
FAC = kN
6.Truss: method of jointsHard
ABBCACACB45 kN25 kN5 m2 m4 m

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

span = 5 mheight = 4 mB is 2 m from Avertical load = 45 kNhorizontal load = 25 kN →
FBC = kN
7.Frames & machinesMedium
OAB300 NQ240 mm120 mmFO​ = ?

The bell crank shown turns about the pin O. A vertical force of 300 N at A (240 mm from O) is balanced by a horizontal force at B (120 mm above O). Find the magnitude of the pin reaction FO.

F = 300 NOA = 240 mmOB = 120 mm
FO = N
8.Frames & machinesHard
F = ?2000 N8 mmABC

A toggle press has two equal links AB and BC, each 80 mm long between pins. The joint B sits 8 mm above the line AC. Which downward force F at B produces a horizontal pressing force of 2000 N at the slider C? Neglect friction and weights.

Q = 2000 NAB = BC = 80 mmh = 8 mm
F = N
9.Shear force & bending momentMedium
w = 4 kN/mP = 55 kNAB1.5 m1 m

The cantilever is fixed at A. It carries a uniformly distributed load w over its whole length and a point load P at 1.5 m from A. Find the bending moment MA at the fixed support A. Use sagging moments positive and upward shear on the left face positive.

L = 2.5 mP = 55 kN at 1.5 mw = 4 kN/m from 0 to 2.5 m
MA = kN·m
10.Shear force & bending momentHard
w = 4 kN/mABC5 m1.5 m

The beam rests on a pin at A and a roller at B and overhangs B by 1.5 m to the free end C. A uniformly distributed load w acts over the whole length A–C. Find the maximum sagging bending moment Mmax between the supports.

L = 6.5 mw = 4 kN/m from 0 to 6.5 msupports at x = 0 and x = 5 m
Mmax = kN·m
11.Centroid & second moment of areaMedium
1802530016xdimensions in mm

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

bf = 180 mmtf = 25 mmtw = 16 mmhw = 300 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2601510012xM = 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 = 260 mmtf = 15 mmtw = 12 mmhw = 100 mmM = 10 kN·m
σtop = MPa

3Solutions

1.Vectors: dot & cross product

Answer: a·b = 16

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.

Multiply matching components and add

a·b = (−5)·(−6) + (−7)·2 + 0·(−1) = 30 + (−14) + 0 = 16

Answer

a·b = 16

Positive: the angle between the vectors is less than 90°.

2.Vectors: dot & cross product

Answer: A = 11.78 m²

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.

Edge vectors

AB = B − A = (1, −2, 5)
AC = C − A = (5, −5, 6)

Cross product

(AB × AC)x = AByACz − ABzACy = (−2)·6 − 5·(−5) = 13
(AB × AC)y = ABzACx − ABxACz = 5·5 − 1·6 = 19
(AB × AC)z = ABxACy − AByACx = 1·(−5) − (−2)·5 = 5
|AB × AC| = √(13² + 19² + 5²) = 23.56

Area of the triangle

A = ½·23.56 = 11.78 m²

Answer

A = 11.78 m²
3.Beam support reactions

Answer: RA = 23.75 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​ = 40 kNABRA​RB​1 m4 m3 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·8 = 10·1 + 40·5
RB = 210/8 = 26.25 kN
ΣFy = 0: RA = 50 − 26.25 = 23.75 kN

Answer

RA = 23.75 kN
4.Beam support reactions

Answer: RA = 33 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 = 5 kN/mP = 30 kNABRA​RB​2 m2 m6 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 = 5·6 = 30 kN, acting at x̄ = 7 m
ΣMA = 0: RB·10 = 30·2 + 5·6·7
RB = 270/10 = 27 kN
ΣFy = 0: RA = 60 − 27 = 33 kN

Answer

RA = 33 kN
5.Truss: method of joints

Answer: FAC = 30 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.

ABBCACACB45 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 45·4 → Cy = 30 kN
ΣFy = 0: Ay = 45 − 30 = 15 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 = 2/2.828 = 0.7071, cos γ = 2/2.828 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −30/0.7071 = −42.43 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−42.43)·0.7071 = 30 kN

Answer

FAC = 30 kN (tension)
6.Truss: method of joints

Answer: FBC = −47.5 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.

ABBCACACB45 kN25 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 45·2 + 25·4 → Cy = 38 kN
ΣFy = 0: Ay = 45 − 38 = 7 kN
ΣFx = 0: Ax = −25 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 = −38/0.8 = −47.5 kN

Answer

FBC = −47.5 kN (compression)
7.Frames & machines

Answer: FO = 670.8 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).

Force at B

Q = 300·240/120 = 600 N

Pin reaction

Ox = 600 N, Oy = 300 N
FO = √(600² + 300²) = 670.8 N

Answer

FO = 670.8 N
8.Frames & machines

Answer: F = 402 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 = 8/80 = 0.1, θ = 5.739°

Link force

Flink = Q/cos θ = 2010 N

Force at B

F = 2·Flink·sin θ = 2·2000·tan θ = 402 N

Answer

F = 402 N
9.Shear force & bending moment

Answer: MA = −95 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.

Keep the free-end part

P: −55·1.5 = −82.5 kN·m
w: −4·2.5²/2 = −12.5 kN·m
MA = −82.5 − 12.5 = −95 kN·m

Answer

MA = −95 kN·m

Negative means hogging: tension on the top face.

10.Shear force & bending moment

Answer: Mmax = 10.35 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 = 4·6.5 = 26 kN, acting at x̄ = 3.25 m
ΣMA = 0: RB·5 = 4·6.5·3.25
RB = 84.5/5 = 16.9 kN
ΣFy = 0: RA = 26 − 16.9 = 9.1 kN

Zero shear

RA − w·x0 = 0 → x0 = 9.1/4 = 2.275 m

Maximum sagging moment

Mmax = RA·x0 − w·x0²/2 = RA²/(2w) = 9.1²/(2·4) = 10.35 kN·m

Answer

Mmax = 10.35 kN·m
11.Centroid & second moment of area

Answer: Ix = 97.57 × 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 two rectangles

Measure every y from the bottom edge.

flange: Af = 180·25 = 4500 mm², yf = 300 + 25/2 = 312.5 mm
web: Aw = 16·300 = 4800 mm², yw = 300/2 = 150 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4500·312.5 + 4800·150)/9300 = 228.6 mm

Parallel-axis theorem

flange: 180·25³/12 + 4500·(312.5 − 228.6)² = 3.189 × 10⁷ mm⁴
web: 16·300³/12 + 4800·(150 − 228.6)² = 6.568 × 10⁷ mm⁴
Ix = 3.189 × 10⁷ + 6.568 × 10⁷ = 9.757 × 10⁷ mm⁴ = 97.57 × 10⁶ mm⁴

Answer

Ix = 97.57 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 51.2 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 = 260·15 = 3900 mm², yf = 100 + 15/2 = 107.5 mm
web: Aw = 12·100 = 1200 mm², yw = 100/2 = 50 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3900·107.5 + 1200·50)/5100 = 93.97 mm

Parallel-axis theorem

flange: 260·15³/12 + 3900·(107.5 − 93.97)² = 787000 mm⁴
web: 12·100³/12 + 1200·(50 − 93.97)² = 3.32 × 10⁶ mm⁴
Ix = 787000 + 3.32 × 10⁶ = 4.107 × 10⁶ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 115 − 93.97 = 21.03 mm
σ = M·y/I = 1 × 10⁷·21.03/4.107 × 10⁶ = 51.2 MPa

Answer

σtop = 51.2 MPa

ExamProblems · examproblems.com/courses/statics