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 value of k for which the vectors a = (2, 6, 2) and b = (−4, k, −4) are perpendicular.

a = (2, 6, 2)b = (−4, k, −4)
k =
2.Vectors: dot & cross productHard
xyzabc

Find the volume V of the parallelepiped whose edges from one corner are a = (−3, 5, −5), b = (−2, 4, −1) and c = (2, 5, −3).

a = (−3, 5, −5)b = (−2, 4, −1)c = (2, 5, −3)
V =
3.Beam support reactionsMedium
w0​ = 8 kN/mP = 45 kNABRA​ = ?3.5 m0.5 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that rises from zero at A to 8 kN/m at B. A point load P also acts at 3.5 m from A. Find the vertical support reaction RA.

L = 4 mw0 = 8 kN/mP = 45 kN at 3.5 m
RA = kN
4.Beam support reactionsHard
w = 5 kN/mP = 70 kNADCMA​ = ?4 m3 m1 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 (8 m from A). It carries a point load P at 7 m from A, a uniformly distributed load w on the whole part CD. Find the magnitude of the reaction moment MA at the wall.

AC = 4 mAD = 8 mP = 70 kN at 7 mw = 5 kN/m from 4 to 8 m
MA = kN·m
5.Truss: method of jointsMedium
ABBCACACB60 kN8 m1 m3 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 = 3 mB is 1 m from Avertical load = 60 kN
FBC = kN
6.Truss: method of jointsHard
ABBCACACB60 kN25 kN5 m1 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 1 m from Avertical load = 60 kNhorizontal load = 25 kN ←
FAC = kN
7.Frames & machinesMedium
10 kN5 m0.8 m1.7 m1.5 mABCDEK

The A-frame shown stands on a pin at A and a roller at B, 5 m apart, with its apex pin C 2.5 m high and the horizontal tie DE 0.8 m above the ground. A vertical load of 10 kN acts on leg AC at K, 1.5 m (horizontally) from A. Find the tension T in the tie.

P = 10 kNAB = 5 mheight of C = 2.5 mheight of DE = 0.8 mhorizontal distance A to K = 1.5 m
T = kN
8.Frames & machinesHard
w = 4 kN/m2 kN1.2 m1.2 m0.6 mABCD

The beam AB of the wall bracket shown is pinned at A and propped by the strut CD (C is 0.6 m below A). The beam carries a uniform load of 4 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 = 4 kN/mP = 2 kNAD = 1.2 mAB = 2.4 mAC = 0.6 m
FCD = kN
9.Shear force & bending momentMedium
M0​ = 30 kN·mAB1.5 m4.5 m

The simply supported beam carries a clockwise couple M0 = 30 kN·m at x = 1.5 m from A, and no other load. Find the bending moment Mx just to the right of the couple. Use sagging moments positive and upward shear on the left face positive.

L = 6 mM0 = 30 kN·m clockwise, at 1.5 m
Mx = kN·m
10.Shear force & bending momentHard
8 kN/m55 kN10 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.

55 kN @ 0 m10 kN @ 6 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)
11.Centroid & second moment of areaMedium
160130t = 14ȳ = ?dimensions in mm

A channel section lies with its open side up: a base plate 160 mm wide with two upright legs, 130 mm high overall. Base and legs are all 14 mm thick. Find the height ȳ of the centroid above the bottom edge.

b = 160 mmh = 130 mmt = 14 mm
ȳ = mm
12.Centroid & second moment of areaHard
3002522018xM = 20 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 20 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 300 mmtf = 25 mmtw = 18 mmhw = 220 mmM = 20 kN·m
σtop = MPa

3Solutions

1.Vectors: dot & cross product

Answer: k = 2.667

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 equals zero

a·b = 2·(−4) + 6·k + 2·(−4) = 0
−16 + 6·k = 0

Solve for k

k = −(−16)/6 = 2.667

Answer

k = 2.667
2.Vectors: dot & cross product

Answer: V = 71

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 = 4·(−3) − (−1)·5 = −7
(b × c)y = bzcx − bxcz = (−1)·2 − (−2)·(−3) = −8
(b × c)z = bxcy − bycx = (−2)·5 − 4·2 = −18

Dot product with a

a·(b × c) = (−3)·(−7) + 5·(−8) + (−5)·(−18) = 71
V = |71| = 71

Answer

V = 71
3.Beam support reactions

Answer: RA = 10.96 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.

Resultant of the triangular load

W = ½·8·4 = 16 kN
x̄ = 2L/3 = 2.667 m

Equilibrium

Moments about A, counter-clockwise positive. Then vertical force balance.

ΣMA = 0: RB·4 = 16·2.667 + 45·3.5
RB = 50.04 kN
RA = 61 − 50.04 = 10.96 kN

Answer

RA = 10.96 kN
4.Beam support reactions

Answer: MA = 110 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.

W = 5·4 = 20 kN at 2 m from C
ΣMC = 0: RD·4 = 70·3 + 20·2
RD = 62.5 kN
VC = 90 − 62.5 = 27.5 kN

Part AC

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

RA = 27.5 = 27.5 kN
MA = 27.5·4 = 110 kN·m

Answer

MA = 110 kN·m
5.Truss: method of joints

Answer: FBC = −19.04 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 = 3/7.616 = 0.3939, cos γ = 7/7.616 = 0.9191
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −7.5/0.3939 = −19.04 kN

Answer

FBC = −19.04 kN (compression)
6.Truss: method of joints

Answer: FAC = −8 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 kN25 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 60·1 − 25·4 → Cy = −8 kN
ΣFy = 0: Ay = 60 − −8 = 68 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 = 4/5.657 = 0.7071, cos γ = 4/5.657 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −−8/0.7071 = 11.31 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(11.31)·0.7071 = −8 kN

Answer

FAC = −8 kN (compression)
7.Frames & machines

Answer: T = 4.412 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.

Whole frame: moments about A

By = 10·1.5/5 = 3 kN

Leg BC: moments about C

3·2.5 = T·1.7
T = 4.412 kN

Answer

T = 4.412 kN
8.Frames & machines

Answer: FCD = 30.41 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 = 4·2.4 = 9.6 kN at 1.2 m

Moments about A for the beam

FCD·0.4472·1.2 = 9.6·1.2 + 2·2.4 = 16.32 kN·m
FCD = 30.41 kN

Answer

FCD = 30.41 kN
9.Shear force & bending moment

Answer: Mx = 22.5 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. An applied couple makes the bending moment diagram jump by the size of the couple.

Support reactions

Moments about A, counter-clockwise positive: RB·L − M0 = 0. Vertical balance: RA + RB = 0.

RB = M0/L = 30/6 = 5 kN (upward)
RA = −RB = −5 kN (downward)

Cut just right of the couple

The left part now contains RA and the couple.

Mx = RA·a + M0 = −5·1.5 + 30 = 22.5 kN·m

Answer

Mx = 22.5 kN·m
10.Shear force & bending moment

Answer: B (x = 1 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 = 78.67 kN, R2 = 10.33 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 = −55 kN·m, MC = −35.33, MD = −23.67, ME = −20, MF = −10, MG = 0

Answer

Mark B: MB = −55 kN·m
11.Centroid & second moment of area

Answer: ȳ = 45.47 mm

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 = 160·14 = 2240 mm², y1 = 7 mm
two legs: A2 = 2·14·116 = 3248 mm², y2 = 14 + 116/2 = 72 mm

Centroid

ȳ = (2240·7 + 3248·72)/5488 = 45.47 mm

Answer

ȳ = 45.47 mm
12.Centroid & second moment of area

Answer: σtop = 19.85 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 = 300·25 = 7500 mm², yf = 220 + 25/2 = 232.5 mm
web: Aw = 18·220 = 3960 mm², yw = 220/2 = 110 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (7500·232.5 + 3960·110)/11460 = 190.2 mm

Parallel-axis theorem

flange: 300·25³/12 + 7500·(232.5 − 190.2)² = 1.383 × 10⁷ mm⁴
web: 18·220³/12 + 3960·(110 − 190.2)² = 4.142 × 10⁷ mm⁴
Ix = 1.383 × 10⁷ + 4.142 × 10⁷ = 5.525 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 245 − 190.2 = 54.83 mm
σ = M·y/I = 2 × 10⁷·54.83/5.525 × 10⁷ = 19.85 MPa

Answer

σtop = 19.85 MPa

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