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
xyzdFAB

A constant force F = (−5, 15, −10) N acts on an object while it moves in a straight line from point A(−2, −4, 3) to point B(3, −3, −2). Coordinates are in metres. Find the work W done by the force.

F = (−5, 15, −10) NA(−2, −4, 3) mB(3, −3, −2) m
W = J
2.Vectors: dot & cross productHard
xyzab

Find the area A of the parallelogram spanned by a = (−4, 4, 3) and b = (−5, −4, 0).

a = (−4, 4, 3)b = (−5, −4, 0)
A =
3.Beam support reactionsMedium
P = 65 kNM = 50 kN·mABRA​ = ?4 m2 m4 m

The simply supported beam has a pin at A and a roller at B. It carries a point load P at 6 m from A and a clockwise couple M at 4 m from A. Find the vertical reaction RA, taking upward as positive.

L = 10 mP = 65 kN at 6 mM = 50 kN·m (clockwise) at 4 m
RA = kN
4.Beam support reactionsHard
w = 3 kN/mP = 30 kNABCRA​ = ?1 m1.5 m2 m1.5 m

The beam has a pin at A and a roller at B, 4.5 m from A, and overhangs B to the free end C. It carries a point load P at 1 m from A and a uniformly distributed load w from 2.5 m to the free end at 6 m. Find the vertical reaction RA, taking upward as positive.

AB = 4.5 mAC = 6 mP = 30 kN at 1 mw = 3 kN/m from 2.5 to 6 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB45 kN4 m3 m4 m

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

span = 4 mheight = 4 mB is 3 m from Avertical load = 45 kN
FBC = kN
6.Truss: method of jointsHard
ABBCACACB50 kN25 kN8 m7 m3 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 = 3 mB is 7 m from Avertical load = 50 kNhorizontal load = 25 kN ←
FAB = kN
7.Frames & machinesMedium
12 kN3 m1 m2.6 mABCDE

The A-frame shown stands on a pin at A and a roller at B, 3 m apart. The legs meet at the pin C, 3.6 m high, and the horizontal tie DE is 1 m above the ground. A load of 12 kN acts at C. Find the magnitude of the force C that the pin C exerts on leg BC.

P = 12 kNAB = 3 mheight of C = 3.6 mheight of DE = 1 m
C = kN
8.Frames & machinesHard
5 kN4.8 m1.2 m3.3 m1.44 mABCDEK

The A-frame shown stands on a pin at A and a roller at B, 4.8 m apart, with its apex pin C 4.5 m high and the horizontal tie DE 1.2 m above the ground. A vertical load of 5 kN acts on leg AC at K, 1.44 m (horizontally) from A. Find the magnitude of the force C that the pin C exerts on leg BC.

P = 5 kNAB = 4.8 mheight of C = 4.5 mheight of DE = 1.2 mhorizontal distance A to K = 1.44 m
C = kN
9.Shear force & bending momentMedium
M0​ = 25 kN·mAB2 m2 m

The simply supported beam carries a clockwise couple M0 = 25 kN·m at x = 2 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 = 4 mM0 = 25 kN·m clockwise, at 2 m
Mx = kN·m
10.Shear force & bending momentHard
w = 10 kN/mP = 45 kNABsection4 m6 m

Find the bending moment Mx at the section x = 4 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mP = 45 kN at 4 mw = 10 kN/m from 0 to 10 mx = 4 m
Mx = kN·m
11.Centroid & second moment of areaMedium
2204602014xdimensions in mm

A symmetric I-section has flanges 220 mm wide and 20 mm thick, an overall depth of 460 mm and a web 14 mm thick. Find its second moment of area Ix about the horizontal centroidal axis x.

B = 220 mmH = 460 mmtf = 20 mmtw = 14 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2402026010xM = 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 bending stress σbottom at the bottom edge.

bf = 240 mmtf = 20 mmtw = 10 mmhw = 260 mmM = 20 kN·m
σbottom = MPa

3Solutions

1.Vectors: dot & cross product

Answer: W = 40 J

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.

Displacement

d = B − A = (3, −3, −2) − (−2, −4, 3) = (5, 1, −5) m

Work

W = F·d = (−5)·5 + 15·1 + (−10)·(−5) = 40 J

Answer

W = 40 J
2.Vectors: dot & cross product

Answer: A = 40.8

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

(a × b)x = aybz − azby = 4·0 − 3·(−4) = 12
(a × b)y = azbx − axbz = 3·(−5) − (−4)·0 = −15
(a × b)z = axby − aybx = (−4)·(−4) − 4·(−5) = 36

Area

A = |a × b| = √(12² + (−15)² + 36²) = 40.8

Answer

A = 40.8
3.Beam support reactions

Answer: RA = 21 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.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·10 − 65·6 − 50 = 0
RB = 440/10 = 44 kN

Vertical equilibrium

RA = 65 − 44 = 21 kN

Answer

RA = 21 kN

A negative reaction acts downward.

4.Beam support reactions

Answer: RA = 23.92 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 distributed load

W = 3·3.5 = 10.5 kN, x̄ = (2.5 + 6)/2 = 4.25 m

Equilibrium

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

ΣMA = 0: RB·4.5 = 30·1 + 10.5·4.25
RB = 74.63/4.5 = 16.58 kN
RA = 40.5 − 16.58 = 23.92 kN

Answer

RA = 23.92 kN
5.Truss: method of joints

Answer: FBC = −34.79 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·4 = 45·3 → 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 = 4/4.123 = 0.9701, cos γ = 1/4.123 = 0.2425
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −33.75/0.9701 = −34.79 kN

Answer

FBC = −34.79 kN (compression)
6.Truss: method of joints

Answer: FAB = −39.67 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.

ABBCACACB50 kN25 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 50·7 − 25·3 → Cy = 34.38 kN
ΣFy = 0: Ay = 50 − 34.38 = 15.63 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 = 3/7.616 = 0.3939
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −15.63/0.3939 = −39.67 kN

Answer

FAB = −39.67 kN (compression)
7.Frames & machines

Answer: C = 6.927 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 = 6 kN
T = 6·1.5/2.6 = 3.462 kN

Components of the pin force on BC

Cx = T = 3.462 kN, Cy = −By = −6 kN

Magnitude

C = √(3.462² + 6²) = 6.927 kN

Answer

C = 6.927 kN
8.Frames & machines

Answer: C = 1.855 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.

Support reaction at B

By = 5·1.44/4.8 = 1.5 kN

Tie force

T = 1.5·2.4/3.3 = 1.091 kN

Pin force on BC

Cx = 1.091 kN, Cy = −1.5 kN
C = √(1.091² + 1.5²) = 1.855 kN

Answer

C = 1.855 kN
9.Shear force & bending moment

Answer: Mx = 12.5 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 = 25/4 = 6.25 kN (upward)
RA = −RB = −6.25 kN (downward)

Cut just right of the couple

The left part now contains RA and the couple.

Mx = RA·a + M0 = −6.25·2 + 25 = 12.5 kN·m

Answer

Mx = 12.5 kN·m
10.Shear force & bending moment

Answer: Mx = 228 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 = 10·10 = 100 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 45·4 + 10·10·5
RB = 680/10 = 68 kN
ΣFy = 0: RA = 145 − 68 = 77 kN
w = 10 kN/mP = 45 kNABRA​ = 77RB​ = 68section4 m6 m

Cut at x = 4 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 = 77·4 − 10·4·2 = 228 kN·m

Answer

Mx = 228 kN·m
11.Centroid & second moment of area

Answer: Ix = 512.6 × 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 − 2·20 = 420 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (220·460³ − 206·420³)/12
Ix = 5.126 × 10⁸ mm⁴ = 512.6 × 10⁶ mm⁴

Answer

Ix = 512.6 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σbottom = 92.27 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 = 240·20 = 4800 mm², yf = 260 + 20/2 = 270 mm
web: Aw = 10·260 = 2600 mm², yw = 260/2 = 130 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4800·270 + 2600·130)/7400 = 220.8 mm

Parallel-axis theorem

flange: 240·20³/12 + 4800·(270 − 220.8)² = 1.177 × 10⁷ mm⁴
web: 10·260³/12 + 2600·(130 − 220.8)² = 3.609 × 10⁷ mm⁴
Ix = 1.177 × 10⁷ + 3.609 × 10⁷ = 4.786 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 220.8 mm
σ = M·y/I = 2 × 10⁷·220.8/4.786 × 10⁷ = 92.27 MPa

Answer

σbottom = 92.27 MPa

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