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 = (6, 2, 6) and b = (1, 6, −5), in degrees.

a = (6, 2, 6)b = (1, 6, −5)
θ = °
2.Vectors: dot & cross productHard
xyzab

For a = (−3, 0, −6) and b = (2, −1, 4), find the z-component (a × b)z of the cross product a × b.

a = (−3, 0, −6)b = (2, −1, 4)
(a × b)z =
3.Beam support reactionsMedium
w = 8 kN/mP = 35 kNABMA​ = ?6 m

The cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w along its whole length and a point load P at 6 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 6 mP = 35 kN at 6 mw = 8 kN/m from 0 to 6 m
MA = kN·m
4.Beam support reactionsHard
P = 35 kN, 50°Q = 30 kNABRA​ = ?2 m2 m4 m

The simply supported beam has a pin at A and a roller at B. A load P acts at 4 m from A, inclined at 50° to the horizontal, and a vertical load Q acts at 2 m from A. Find the magnitude of the total reaction force RA at the pin A.

L = 8 mP = 35 kN at 4 m, θ = 50°Q = 30 kN at 2 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB45 kN8 m6 m4 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 = 4 mB is 6 m from Avertical load = 45 kN
FBC = kN
6.Truss: method of jointsHard
ABCDEFGH35 kN20 kN15 kN30 kN25 kN4 × 3 m4 m

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

C: 35 kN ↓D: 20 kN ↓F: 15 kN ↓G: 30 kN ↓H: 25 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
20 kN6 m1.5 m2.1 mABCDE

The A-frame shown stands on a pin at A and a roller at B, 6 m apart. The legs meet at the pin C, 3.6 m high, and the horizontal tie DE is 1.5 m above the ground. A load of 20 kN acts at C. Find the magnitude of the force C that the pin C exerts on leg BC.

P = 20 kNAB = 6 mheight of C = 3.6 mheight of DE = 1.5 m
C = kN
8.Frames & machinesHard
2 kN2 kN5 m3 mABC

A uniform horizontal boom AB of weight 2 kN is pinned to a wall at A and held by a cable from its end B to the point C on the wall, 3 m above A. A load of 2 kN hangs at B. Find the tension T in the cable.

W = 2 kNWb = 2 kNAB = 5 mAC = 3 m
T = kN
9.Shear force & bending momentMedium
P1​ = 45 kNP2​ = 30 kNABC4 m4 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. It carries a point load P1 between the supports and a point load P2 at C. Find the bending moment Mx under the load P1. Use sagging moments positive and upward shear on the left face positive.

L = 9.5 mP1 = 45 kN at 4 mP2 = 30 kN at 9.5 msupports at x = 0 and x = 8 m
Mx = kN·m
10.Shear force & bending momentHard
w = 6 kN/mP = 35 kNABsection3.5 m2.5 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 = 6 mP = 35 kN at 3.5 mw = 6 kN/m from 0 to 6 mx = 3.5 m
Mx = kN·m
11.Centroid & second moment of areaMedium
300301208xdimensions in mm

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

bf = 300 mmtf = 30 mmtw = 8 mmhw = 120 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
190340106xM = 80 kN·mdimensions in mm

A symmetric I-section has flanges 190 mm wide and 10 mm thick, an overall depth of 340 mm and a web 6 mm thick. It carries a bending moment of 80 kN·m about the axis x. Find the size of the bending stress σj at the junction of the web and the top flange.

B = 190 mmH = 340 mmtf = 10 mmtw = 6 mmM = 80 kN·m
σj = MPa

3Solutions

1.Vectors: dot & cross product

Answer: θ = 100.1 °

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 = 6·1 + 2·6 + 6·(−5) = −12

Magnitudes

|a| = √(6² + 2² + 6²) = 8.718
|b| = √(1² + 6² + (−5)²) = 7.874

Angle

cos θ = −12/(8.718·7.874) = −0.1748
θ = arccos(−0.1748) = 100.1°

Answer

θ = 100.1°
2.Vectors: dot & cross product

Answer: (a × b)z = 3

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 = 0·4 − (−6)·(−1) = −6
(a × b)y = azbx − axbz = (−6)·2 − (−3)·4 = 0
(a × b)z = axby − aybx = (−3)·(−1) − 0·2 = 3

Requested component

(a × b)z = 3

Answer

(a × b)z = 3

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

3.Beam support reactions

Answer: MA = 354 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 distributed load

W = 8·6 = 48 kN, x̄ = 3 m

Moment about the wall

MA = P·a + W·x̄ = 35·6 + 48·3 = 354 kN·m

Answer

MA = 354 kN·m
4.Beam support reactions

Answer: RA = 42.37 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.

Components of P

Pv = 35·sin 50° = 26.81 kN
Ph = 35·cos 50° = 22.5 kN

Reactions

ΣMA = 0: RB·8 = 26.81·4 + 30·2 → RB = 20.91 kN
Ay = 26.81 + 30 − 20.91 = 35.91 kN
Ax = Ph = 22.5 kN

Resultant at A

RA = √(22.5² + 35.91²) = 42.37 kN

Answer

RA = 42.37 kN
5.Truss: method of joints

Answer: FBC = −37.73 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 = 45·6 → Cy = 33.75 kN
ΣFy = 0: Ay = 45 − 33.75 = 11.25 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 = 4/4.472 = 0.8944, cos γ = 2/4.472 = 0.4472
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −33.75/0.8944 = −37.73 kN

Answer

FBC = −37.73 kN (compression)
6.Truss: method of joints

Answer: member BF

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 B

AB and BC lie on one straight line and the joint carries no load. Balancing forces across that line leaves only BF.

ΣF⊥ = 0 → FBF = 0

Check with the method of joints

Solving all joints gives these member forces (T = tension, C = compression).

AB: 17.81 kN (T), BC: 17.81 kN (T), CD: 32.19 kN (T), DE: 32.19 kN (T), FG: 74.38 kN (C), GH: 74.38 kN (C), AF: 71.35 kN (C), HE: 53.65 kN (C), BF: 0, CG: 30 kN (C), DH: 20 kN (T), FC: 52.6 kN (T), HC: 28.65 kN (T)

Answer

Zero-force member: BF
7.Frames & machines

Answer: C = 17.44 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.

Tie force from leg BC

By = 10 kN
T = 10·3/2.1 = 14.29 kN

Components of the pin force on BC

Cx = T = 14.29 kN, Cy = −By = −10 kN

Magnitude

C = √(14.29² + 10²) = 17.44 kN

Answer

C = 17.44 kN
8.Frames & machines

Answer: T = 5.831 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 = √(5² + 3²) = 5.831 m, sin β = 0.5145

Moments about A

T·0.5145·5 = 2·5 + 2·2.5
T = 5.831 kN

Answer

T = 5.831 kN
9.Shear force & bending moment

Answer: Mx = 67.5 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. The overhang load also acts about A.

ΣMA = 0: RB·8 = 45·4 + 30·9.5
RB = 465/8 = 58.13 kN
ΣFy = 0: RA = 75 − 58.13 = 16.88 kN

Cut under P1 and keep the left part

Mx = RA·4 = 16.88·4 = 67.5 kN·m

Answer

Mx = 67.5 kN·m
10.Shear force & bending moment

Answer: Mx = 77.29 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 = 6·6 = 36 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 35·3.5 + 6·6·3
RB = 230.5/6 = 38.42 kN
ΣFy = 0: RA = 71 − 38.42 = 32.58 kN
w = 6 kN/mP = 35 kNABRA​ = 32.58RB​ = 38.42section3.5 m2.5 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 = 32.58·3.5 − 6·3.5·1.75 = 77.29 kN·m

Answer

Mx = 77.29 kN·m
11.Centroid & second moment of area

Answer: Ix = 6.707 × 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 = 300·30 = 9000 mm², yf = 120 + 30/2 = 135 mm
web: Aw = 8·120 = 960 mm², yw = 120/2 = 60 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (9000·135 + 960·60)/9960 = 127.8 mm

Parallel-axis theorem

flange: 300·30³/12 + 9000·(135 − 127.8)² = 1.145 × 10⁶ mm⁴
web: 8·120³/12 + 960·(60 − 127.8)² = 5.561 × 10⁶ mm⁴
Ix = 1.145 × 10⁶ + 5.561 × 10⁶ = 6.707 × 10⁶ mm⁴ = 6.707 × 10⁶ mm⁴

Answer

Ix = 6.707 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σj = 106.8 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 = 340 − 2·10 = 320 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (190·340³ − 184·320³)/12
Ix = 1.199 × 10⁸ mm⁴

Bending stress

y = 170 − 10 = 160 mm
σ = M·y/I = 8 × 10⁷·160/1.199 × 10⁸ = 106.8 MPa

Answer

σj = 106.8 MPa

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