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 = (−20, 0, 30) N acts on an object while it moves in a straight line from point A(2, 0, 1) to point B(−2, −4, 0). Coordinates are in metres. Find the work W done by the force.

F = (−20, 0, 30) NA(2, 0, 1) mB(−2, −4, 0) m
W = J
2.Vectors: dot & cross productHard
xyzrFOA

A force F = (−10, −60, 0) N acts at point A(−3, −3, 1). Coordinates are in metres. Find the magnitude |M| of the moment of the force about point O(−2, −1, −3).

F = (−10, −60, 0) NA(−3, −3, 1) mO(−2, −1, −3) m
|M| = N·m
3.Beam support reactionsMedium
w = 6 kN/mP = 45 kNABRA​ = ?2 m3 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 2 m from the wall. Find the vertical reaction RA at the wall.

L = 5 mP = 45 kN at 2 mw = 6 kN/m from 0 to 5 m
RA = kN
4.Beam support reactionsHard
w = 10 kN/mP = 40 kNABRA​ = ?RB​1.5 m3.5 m

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

L = 5 mP = 40 kN at 1.5 mw = 10 kN/m from 0 to 5 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB25 kN8 m5 m2 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 = 2 mB is 5 m from Avertical load = 25 kN
FAC = kN
6.Truss: method of jointsHard
ABBCACACB25 kN25 kN5 m2 m4 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 = 4 mB is 2 m from Avertical load = 25 kNhorizontal load = 25 kN ←
FAB = kN
7.Frames & machinesMedium
OAB150 NQ240 mm100 mmFO​ = ?

The bell crank shown turns about the pin O. A vertical force of 150 N at A (240 mm from O) is balanced by a horizontal force at B (100 mm above O). Find the magnitude of the pin reaction FO.

F = 150 NOA = 240 mmOB = 100 mm
FO = N
8.Frames & machinesHard
10 kN5 m0.8 m1.7 mABCDE

The A-frame shown stands on a pin at A and a roller at B, 5 m apart. The legs meet at the pin C, 2.5 m high, and are tied by the horizontal bar DE at 0.8 m. A horizontal force of 10 kN to the right acts at C. Find the tension T in the tie.

P = 10 kNAB = 5 mheight of C = 2.5 mheight of DE = 0.8 m
T = kN
9.Shear force & bending momentMedium
P1​ = 25 kNP2​ = 80 kNABC2 m6 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 MB at support B. Use sagging moments positive and upward shear on the left face positive.

L = 9.5 mP1 = 25 kN at 2 mP2 = 80 kN at 9.5 msupports at x = 0 and x = 8 m
MB = kN·m
10.Shear force & bending momentHard
w = 5 kN/mP = 20 kNABsection3 m1 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 = 4 mP = 20 kN at 3 mw = 5 kN/m from 0 to 4 mx = 3 m
Mx = kN·m
11.Centroid & second moment of areaMedium
2602010010xdimensions in mm

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

bf = 260 mmtf = 20 mmtw = 10 mmhw = 100 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2802026012xM = 25 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 25 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 280 mmtf = 20 mmtw = 12 mmhw = 260 mmM = 25 kN·m
σbottom = MPa

3Solutions

1.Vectors: dot & cross product

Answer: W = 50 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 = (−2, −4, 0) − (2, 0, 1) = (−4, −4, −1) m

Work

W = F·d = (−20)·(−4) + 0·(−4) + 30·(−1) = 50 J

Answer

W = 50 J
2.Vectors: dot & cross product

Answer: |M| = 246.6 N·m

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.

Position vector from O to A

r = A − O = (−3, −3, 1) − (−2, −1, −3) = (−1, −2, 4) m

Moment M = r × F

(r × F)x = ryFz − rzFy = (−2)·0 − 4·(−60) = 240 N·m
(r × F)y = rzFx − rxFz = 4·(−10) − (−1)·0 = −40 N·m
(r × F)z = rxFy − ryFx = (−1)·(−60) − (−2)·(−10) = 40 N·m

Magnitude

|M| = √(240² + (−40)² + 40²) = 246.6 N·m

Answer

|M| = 246.6 N·m
3.Beam support reactions

Answer: RA = 75 kN

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 = 6·5 = 30 kN, x̄ = 2.5 m

Vertical equilibrium

RA = P + W = 45 + 30 = 75 kN

Answer

RA = 75 kN
4.Beam support reactions

Answer: RA = 53 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 = 10 kN/mP = 40 kNABRA​RB​1.5 m3.5 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.

UDL resultant: W = w·ℓ = 10·5 = 50 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 40·1.5 + 10·5·2.5
RB = 185/5 = 37 kN
ΣFy = 0: RA = 90 − 37 = 53 kN

Answer

RA = 53 kN
5.Truss: method of joints

Answer: FAC = 23.44 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.

ABBCACACB25 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 25·5 → Cy = 15.63 kN
ΣFy = 0: Ay = 25 − 15.63 = 9.375 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 = 2/3.606 = 0.5547, cos γ = 3/3.606 = 0.8321
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −15.63/0.5547 = −28.17 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−28.17)·0.8321 = 23.44 kN

Answer

FAC = 23.44 kN (tension)
6.Truss: method of joints

Answer: FAB = −39.13 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.

ABBCACACB25 kN25 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 25·2 − 25·4 → Cy = −10 kN
ΣFy = 0: Ay = 25 − −10 = 35 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 = 4/4.472 = 0.8944
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −35/0.8944 = −39.13 kN

Answer

FAB = −39.13 kN (compression)
7.Frames & machines

Answer: FO = 390 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 = 150·240/100 = 360 N

Pin reaction

Ox = 360 N, Oy = 150 N
FO = √(360² + 150²) = 390 N

Answer

FO = 390 N
8.Frames & machines

Answer: T = 7.353 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·5 = 10·2.5
By = 5 kN

Leg BC: moments about C

5·2.5 = T·1.7
T = 7.353 kN

Answer

T = 7.353 kN

A positive T means the tie is in tension, as assumed.

9.Shear force & bending moment

Answer: MB = −120 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 = 25·2 + 80·9.5
RB = 810/8 = 101.3 kN
ΣFy = 0: RA = 105 − 101.3 = 3.75 kN

Cut at B and keep the overhang

Only P2 acts on the overhang, with lever arm a. It bends the beam upward over the support (hogging).

MB = −P2·a = −80·1.5 = −120 kN·m

Answer

MB = −120 kN·m
10.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.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 5·4 = 20 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 20·3 + 5·4·2
RB = 100/4 = 25 kN
ΣFy = 0: RA = 40 − 25 = 15 kN
w = 5 kN/mP = 20 kNABRA​ = 15RB​ = 25section3 m1 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 = 15·3 − 5·3·1.5 = 22.5 kN·m

Answer

Mx = 22.5 kN·m
11.Centroid & second moment of area

Answer: Ix = 4.026 × 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 = 260·20 = 5200 mm², yf = 100 + 20/2 = 110 mm
web: Aw = 10·100 = 1000 mm², yw = 100/2 = 50 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (5200·110 + 1000·50)/6200 = 100.3 mm

Parallel-axis theorem

flange: 260·20³/12 + 5200·(110 − 100.3)² = 660326 mm⁴
web: 10·100³/12 + 1000·(50 − 100.3)² = 3.366 × 10⁶ mm⁴
Ix = 660326 + 3.366 × 10⁶ = 4.026 × 10⁶ mm⁴ = 4.026 × 10⁶ mm⁴

Answer

Ix = 4.026 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σbottom = 96.39 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 = 280·20 = 5600 mm², yf = 260 + 20/2 = 270 mm
web: Aw = 12·260 = 3120 mm², yw = 260/2 = 130 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (5600·270 + 3120·130)/8720 = 219.9 mm

Parallel-axis theorem

flange: 280·20³/12 + 5600·(270 − 219.9)² = 1.424 × 10⁷ mm⁴
web: 12·260³/12 + 3120·(130 − 219.9)² = 4.28 × 10⁷ mm⁴
Ix = 1.424 × 10⁷ + 4.28 × 10⁷ = 5.703 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 219.9 mm
σ = M·y/I = 2.5 × 10⁷·219.9/5.703 × 10⁷ = 96.39 MPa

Answer

σbottom = 96.39 MPa

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