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 scalar projection compb a of a = (−4, −7, −1) onto b = (5, 2, −2), that is, the component of a in the direction of b.

a = (−4, −7, −1)b = (5, 2, −2)
compb a =
2.Vectors: dot & cross productHard
xyzab

For a = (−1, 5, −6) and b = (−5, 2, 6), find the x-component (a × b)x of the cross product a × b.

a = (−1, 5, −6)b = (−5, 2, 6)
(a × b)x =
3.Beam support reactionsMedium
P1​ = 25 kNP2​ = 50 kNABRA​ = ?RB​3 m0.5 m1.5 m

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

L = 5 mP1 = 25 kN at 3 mP2 = 50 kN at 3.5 m
RA = kN
4.Beam support reactionsHard
w = 2 kN/mP = 15 kNABRA​ = ?RB​2 m3 m1 m

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

L = 6 mP = 15 kN at 5 mw = 2 kN/m from 2 to 5 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB45 kN8 m7 m3 m

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

span = 8 mheight = 3 mB is 7 m from Avertical load = 45 kN
FAC = kN
6.Truss: method of jointsHard
ABBCACACB35 kN25 kN5 m2 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 2 m from Avertical load = 35 kNhorizontal load = 25 kN →
FAB = kN
7.Frames & machinesMedium
8 kN0.75 m1.65 m0.8 mABCD

A horizontal beam AB is pinned to a wall at A and propped by the strut CD, pinned to the wall at C, 0.8 m below A. A load of 8 kN hangs at B. Neglect the weights. Find the magnitude of the pin force A on the beam at A.

P = 8 kNAD = 0.75 mAB = 2.4 mAC = 0.8 m
A = kN
8.Frames & machinesHard
12 kN1.5 kN2 m2 mABC

A uniform horizontal boom AB of weight 1.5 kN is pinned to a wall at A and held by a cable from B to the point C on the wall, 2 m above A. A load of 12 kN hangs at B. Find the magnitude of the pin reaction A.

W = 12 kNWb = 1.5 kNAB = 2 mAC = 2 m
A = kN
9.Shear force & bending momentMedium
w = 2 kN/mABsection2.5 m5.5 m

Find the shear force Vx at the section x = 2.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mw = 2 kN/m from 0 to 8 mx = 2.5 m
Vx = kN
10.Shear force & bending momentHard
w = 3 kN/mP = 35 kNABsection3 m0.5 m2.5 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 mP = 35 kN at 3.5 mw = 3 kN/m from 0 to 6 mx = 3 m
Mx = kN·m
11.Centroid & second moment of areaMedium
150 mm240 mm144 mmØ50xIx​ = ?

A 150 mm × 240 mm plate has a circular hole of diameter 50 mm on its vertical centre line, with its centre 144 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 150 mmh = 240 mmd = 50 mmhole centre: y = 144 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
190500248xM = 50 kN·mdimensions in mm

A symmetric I-section has flanges 190 mm wide and 24 mm thick, an overall depth of 500 mm and a web 8 mm thick. It carries a bending moment of 50 kN·m about the axis x. Find the size of the maximum bending stress σmax in the section.

B = 190 mmH = 500 mmtf = 24 mmtw = 8 mmM = 50 kN·m
σmax = MPa

3Solutions

1.Vectors: dot & cross product

Answer: compb a = −5.57

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 = (−4)·5 + (−7)·2 + (−1)·(−2) = −32

Length of b

|b| = √(5² + 2² + (−2)²) = 5.745

Scalar projection

compb a = a·b/|b| = −32/5.745 = −5.57

Answer

compb a = −5.57

Negative: a has a component pointing against b.

2.Vectors: dot & cross product

Answer: (a × b)x = 42

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, component by component

(a × b)x = aybz − azby = 5·6 − (−6)·2 = 42
(a × b)y = azbx − axbz = (−6)·(−5) − (−1)·6 = 36
(a × b)z = axby − aybx = (−1)·2 − 5·(−5) = 23

Requested component

(a × b)x = 42

Answer

(a × b)x = 42

Check: a × b is perpendicular to both vectors, so its dot product with a and with b is zero.

3.Beam support reactions

Answer: RA = 25 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​ = 25 kNP2​ = 50 kNABRA​RB​3 m0.5 m1.5 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.

ΣMA = 0: RB·5 = 25·3 + 50·3.5
RB = 250/5 = 50 kN
ΣFy = 0: RA = 75 − 50 = 25 kN

Answer

RA = 25 kN
4.Beam support reactions

Answer: RA = 5 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 = 2 kN/mP = 15 kNABRA​RB​2 m3 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.

UDL resultant: W = w·ℓ = 2·3 = 6 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·6 = 15·5 + 2·3·3.5
RB = 96/6 = 16 kN
ΣFy = 0: RA = 21 − 16 = 5 kN

Answer

RA = 5 kN
5.Truss: method of joints

Answer: FAC = 13.13 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·8 = 45·7 → Cy = 39.38 kN
ΣFy = 0: Ay = 45 − 39.38 = 5.625 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 = 3/3.162 = 0.9487, cos γ = 1/3.162 = 0.3162
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −39.38/0.9487 = −41.5 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−41.5)·0.3162 = 13.13 kN

Answer

FAC = 13.13 kN (tension)
6.Truss: method of joints

Answer: FAB = −15.56 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 kN25 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 35·2 + 25·2 → Cy = 24 kN
ΣFy = 0: Ay = 35 − 24 = 11 kN
ΣFx = 0: Ax = −25 kN

Joint A

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

sin α = 2/2.828 = 0.7071
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −11/0.7071 = −15.56 kN

Answer

FAB = −15.56 kN (compression)
7.Frames & machines

Answer: A = 29.76 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 = 8·2.4/(0.7295·0.75) = 35.09 kN

Components at A

Ax = FCD·cos α = 24 kN (towards the wall)
Ay = 8 − FCD·sin α = −17.6 kN

Magnitude

A = √(24² + −17.6²) = 29.76 kN

Answer

A = 29.76 kN

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

8.Frames & machines

Answer: A = 12.77 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 tension

T = (12 + 1.5/2)/0.7071 = 18.03 kN

Components at A

Ax = T·cos β = 12.75 kN
Ay = 12 + 1.5 − T·sin β = 0.75 kN

Magnitude

A = √(12.75² + 0.75²) = 12.77 kN

Answer

A = 12.77 kN
9.Shear force & bending moment

Answer: Vx = 3 kN

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 = 2·8 = 16 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 2·8·4
RB = 64/8 = 8 kN
ΣFy = 0: RA = 16 − 8 = 8 kN
w = 2 kN/mABRA​ = 8RB​ = 8section2.5 m5.5 m

Cut at x = 2.5 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.

V = RA − (all downward loads left of the cut)
Vx = 8 − 2·2.5 = 3 kN

Answer

Vx = 3 kN
10.Shear force & bending moment

Answer: Mx = 57.25 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.

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 = 35·3.5 + 3·6·3
RB = 176.5/6 = 29.42 kN
ΣFy = 0: RA = 53 − 29.42 = 23.58 kN
w = 3 kN/mP = 35 kNABRA​ = 23.58RB​ = 29.42section3 m0.5 m2.5 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 = 23.58·3 − 3·3·1.5 = 57.25 kN·m

Answer

Mx = 57.25 kN·m
11.Centroid & second moment of area

Answer: Ix = 171.3 × 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 = (36000·120 − 1963·144)/(36000 − 1963) = 118.6 mm

Full plate about ȳ

150·240³/12 + 36000·1.385² = 172.9 × 10⁶ mm⁴

Hole about ȳ

π·50⁴/64 + 1963·25.38² = 1.572 × 10⁶ mm⁴

Subtract

Ix = 171.3 × 10⁶ mm⁴

Answer

Ix = 171.3 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σmax = 21.6 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.

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 = 500 − 2·24 = 452 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (190·500³ − 182·452³)/12
Ix = 5.786 × 10⁸ mm⁴

Bending stress

y = 250 mm
σ = M·y/I = 5 × 10⁷·250/5.786 × 10⁸ = 21.6 MPa

Answer

σmax = 21.6 MPa

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