FE Civil exam practice: cram pack

Formula sheets, the key method steps for every topic and 30 practice problems, with full solutions at the back.

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1Formulas and methods

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.

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.

Beam deflection

Point load at midspan
δ = PL³/(48EI)
Uniform load, simply supported
δ = 5wL⁴/(384EI)
Cantilever, end load
δ = PL³/(3EI)
Cantilever, uniform load
δ = wL⁴/(8EI)
Superposition
δ = δ1 + δ2

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

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)

Effective stress in soil

Total stress
σ = Σγi·hi
Pore water pressure
u = γw·(z − zw)
Effective stress
σ′ = σ − u
Water
γw = 9.81 kN/m³

Consolidation settlement

Normally consolidated
S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0)
Final stress
σ′f = σ′0 + Δσ (at mid-depth of the layer)
Overconsolidated, σ′f ≤ σ′p
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0)
Overconsolidated, σ′f > σ′p
S = H/(1 + e0)·[Cr·log₁₀(σ′p/σ′0) + Cc·log₁₀(σ′f/σ′p)]
Overconsolidation ratio
OCR = σ′p/σ′0
Time for consolidation
t = Tv·Hdr²/cv
Drainage path
Hdr = H/2 (double drainage), H (single drainage)
Time factors
U 50% → 0.197, 60% → 0.287, 70% → 0.403, 80% → 0.567, 90% → 0.848

Hydrostatic force

Pressure at depth
p = ρgh
Force on a vertical wall
F = ρg·hc·A
Centre of pressure
yp = yc + Ic/(ycA)
Rectangle
Ic = bH³/12

Pipe friction & head loss

Reynolds number
Re = V·D/ν = ρ·V·D/μ
Flow regime
laminar below Re ≈ 2000, turbulent above Re ≈ 4000
Mean velocity
V = Q/A, A = π·D²/4
Darcy–Weisbach
hf = f·(L/D)·V²/(2g)
Minor losses
hm = ΣK·V²/(2g)
Typical K values
entrance 0.5, exit 1.0, 90° bend ≈ 0.3
Pressure drop
Δp = ρ·g·hf
Two open reservoirs
Δz = (f·L/D + ΣK)·V²/(2g)
Free outlet
H = (1 + f·L/D + ΣK)·V²/(2g)

Open-channel flow (Manning)

Manning equation
V = (1/n)·R2/3·S1/2
Flow rate
Q = A·V
Hydraulic radius
R = A/P (P = wetted perimeter, free surface excluded)
Rectangle
A = b·y, P = b + 2y
Trapezoid (side slope z:1)
A = (b + z·y)·y, P = b + 2y·√(1 + z²)
Circular pipe, full or half full
R = D/4
Required slope
S = (n·Q/(A·R2/3))²

Pumps & pump power

Hydraulic power
Ph = ρ·g·Q·H = Q·Δp
Shaft power
Pshaft = Ph/ηpump
Electrical power
Pel = Pshaft/ηmotor
Pump head
H = Δz + Δp/(ρ·g) + hL
System losses
hL = (f·L/D + ΣK)·V²/(2g)

Time value of money

Future value
FV = PV·(1 + i)n
Present value
PV = FV/(1 + i)n
Several periods per year
i = r/m, N = m·n
Annuity, present value
PV = PMT·[1 − (1 + i)−n]/i
Annuity, future value
FV = PMT·[(1 + i)n − 1]/i

Method

  1. Draw a timeline with every cash flow and its timing.
  2. Match the rate to the period: a monthly rate for monthly payments.
  3. Use FV = PV·(1 + i)ⁿ for single amounts and the annuity formulas for equal payments.
  4. Check the sign and the order of magnitude of the answer.

NPV & IRR

Net present value
NPV = −C0 + Σ CFt/(1 + r)t
Equal cash flows
NPV = −C0 + CF·[1 − (1 + r)−n]/r
Internal rate of return
the r at which NPV = 0
Decision
accept when NPV > 0 (or IRR > required return)

Method

  1. List all cash flows with their year; the investment at year 0 is negative.
  2. Discount each cash flow: CFt/(1 + r)t.
  3. Add them up to get the NPV. Positive means the project earns more than r.
  4. For the IRR, find the rate that makes NPV zero by trial or interpolation.

Normal distribution

z-score
z = (x − μ)/σ
Below x
P(X < x) = Φ(z)
Above x
P(X > x) = 1 − Φ(z)
Between
Φ(z2) − Φ(z1)
Percentile
x = μ + z·σ

Method

  1. Convert the value to a z-score: z = (x − μ)/σ.
  2. Look up Φ(z), the area to the left of z.
  3. For the area to the right use 1 − Φ(z); for an interval subtract the two left areas.
  4. For a percentile, work backwards: find z for the area, then x = μ + z·σ.

2Practice problems

1.Beam support reactionsMedium
P1​ = 50 kNP2​ = 50 kNABRA​RB​ = ?3 m1 m1 m

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

L = 5 mP1 = 50 kN at 3 mP2 = 50 kN at 4 m
RB = kN
2.Beam support reactionsHard
w = 6 kN/mP = 65 kNABCRA​ = ?2.5 m1 m1.5 m

The beam has a pin at A and a roller at B, 3.5 m from A, and overhangs B to the free end C. It carries a point load P at 2.5 m from A and a uniformly distributed load w from 3.5 m to the free end at 5 m. Find the vertical reaction RA, taking upward as positive.

AB = 3.5 mAC = 5 mP = 65 kN at 2.5 mw = 6 kN/m from 3.5 to 5 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB50 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 = 50 kN
FBC = kN
4.Truss: method of jointsHard
ABCDEFGH35 kN25 kN15 kN40 kN4 × 4 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.

B: 35 kN ↓F: 25 kN ↓F: 15 kN →G: 40 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 BG
  13. 13member DG
5.Shear force & bending momentMedium
w = 3 kN/mABsection3.5 m2.5 m

Find the shear force Vx at the section x = 3.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 6 mw = 3 kN/m from 0 to 6 mx = 3.5 m
Vx = kN
6.Shear force & bending momentHard
6 kN/m30 kN60 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.

30 kN @ 6 m60 kN @ 1 m6 kN/m, 0–5 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)
7.Beam deflectionMedium
w = 5 kN/mδL = 1.5 m

A cantilever carries a uniformly distributed load w over its whole length. Find the deflection δ at the free end.

w = 5 kN/mL = 1.5 mE = 11 GPa (timber)I = 120 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 2 kN/mABδ4 m

A simply supported timber beam of rectangular section, 100 mm wide, carries a uniformly distributed load w over its whole span. Its midspan deflection may not exceed span/250. Find the smallest depth hreq of the section.

w = 2 kN/mL = 4 mE = 11 GPa (timber)b = 100 mm
hreq = mm
9.Column bucklingMedium
PL = 4 m40 × 80 mmcross-section

A column of length L made of steel is fixed at the base and pinned at the top. Using Euler’s formula, find its critical buckling load Pcr.

L = 4 mE = 200 GPa (steel)b × h = 40 × 80 mm
Pcr = kN
10.Column bucklingHard
PL = 5 md = 60 mmcross-section

A column of length L made of aluminium is fixed at the base and pinned at the top. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 5 mE = 70 GPa (aluminium)d = 60 mm
σcr = MPa
11.Centroid & second moment of areaMedium
2002801010xdimensions in mm

A symmetric I-section has flanges 200 mm wide and 10 mm thick, an overall depth of 280 mm and a web 10 mm thick. Find its second moment of area Ix about the horizontal centroidal axis x.

B = 200 mmH = 280 mmtf = 10 mmtw = 10 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
120360208xM = 80 kN·mdimensions in mm

A symmetric I-section has flanges 120 mm wide and 20 mm thick, an overall depth of 360 mm and a web 8 mm thick. It carries a bending moment of 80 kN·m about the axis x. Find the size of the maximum bending stress σmax in the section.

B = 120 mmH = 360 mmtf = 20 mmtw = 8 mmM = 80 kN·m
σmax = MPa
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 19.5 kN/m³8 mwater tableXz = 4 m

For the soil profile shown, find the vertical effective stress σ′ at point X.

z = 4 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16.5 kN/m³γsat​ = 19 kN/m³5 mclayγsat​ = 17 kN/m³4 mwater tableXz = 7 m

For the soil profile shown, find the vertical effective stress σ′ at point X.

z = 7 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19 kN/m³clay: γsat = 17 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 65 kPasandclayCc​ = 0.4, Cr​ = 0.06e0​ = 1.1σ′0​ = 90 kPaσ′p​ = 160 kPa8 mwater table

An 8 m thick overconsolidated clay layer has Cc = 0.4, Cr = 0.06 and e₀ = 1.1. At its mid-depth the effective vertical stress is 90 kPa and the preconsolidation pressure is 160 kPa. A new building adds 65 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 8 mCc = 0.4Cr = 0.06e0 = 1.1σ′0 = 90 kPaσ′p = 160 kPaΔσ = 65 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 7 mcv​ = 5 m²/year7 msandwater table

A clay layer 7 m thick has a coefficient of consolidation cv = 5 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 90% average consolidation the time factor is Tv = 0.848. How many years t does the layer take to reach 90% consolidation?

H = 7 mcv = 5 m²/yearU = 90%Tv = 0.848double drainage
t = years
17.Hydrostatic forceMedium
gated = 2.5 mH = 2.5 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 2.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2.5 mH = 2.5 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2.5 mH = 3 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of glycerin, with its top edge 2.5 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 2.5 mH = 3 mb = 2 mρ = 1260 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 0.8 m/sD = 150 mmL = 500 mf = 0.028

Water flows at a mean velocity of 0.8 m/s through a pipe 500 m long with an inside diameter of 150 mm. Use the Darcy friction factor f = 0.028 and g = 9.81 m/s². Find the friction head loss hf.

V = 0.8 m/sL = 500 mD = 150 mmf = 0.028g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2free outletH = ?L = 200 m, D = 200 mm, f = 0.0224× bend (K = 0.3)

A pipe 200 m long with an inside diameter of 200 mm (Darcy friction factor f = 0.022) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each) and a valve (K = 2). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 40 L/s?

Q = 40 L/sL = 200 mD = 200 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 2
H = m
21.Open-channel flow (Manning)Medium
b = 1.5 my = 1.4 m3 : 1n = 0.015, S = 0.0005

A trapezoidal brickwork channel has a bottom width of 1.5 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 1.4 m deep. Manning n = 0.015 and the bed slope is S = 0.0005. Find the flow rate Q in m³/s.

b = 1.5 my = 1.4 mz = 3n = 0.015S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 375 mmn = 0.013, V = 0.75 m/s

A concrete sewer with an inside diameter of 375 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.75 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 375 mmn = 0.013V = 0.75 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 40 L/sH = 72 m

A pump delivers 40 L/s of water (ρ = 1000 kg/m³) against a head of 72 m. The pump efficiency is 72% and the electric motor driving it has an efficiency of 88%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 40 L/sH = 72 mηpump = 72%ηmotor = 88%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
400 kPa (gauge)PQ = 20 L/sΔz = 7 mL = 400 m, D = 100 mm, f = 0.025, ΣK = 8

A pump moves 20 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 7 m higher. The pipe is 400 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 400 kPa. Find the head H the pump must add.

Q = 20 L/sΔz = 7 mL = 400 mD = 100 mmf = 0.025ΣK = 8ptank = 400 kPa
H = m
25.Time value of moneyMedium
years0123…10€20 000FV = ?

You invest €20 000 at 7% per year with continuous compounding. Find the value FV after 10 years.

PV = €20 000r = 7%t = 10
FV = €
26.Time value of moneyHard
months0123…84€250€250€250FV = ?

You save €250 at the end of every month for 7 years. The account pays 2.4% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €2502.4% / 12N = 84
FV = €
27.NPV & IRRMedium
years012345−40 0009 0009 0009 0009 00017 000

A machine costs €40 000 today. It generates €9 000 at the end of each year for 5 years and can then be sold for €8 000. The cost of capital is 6%. Find the net present value NPV.

C0 = €40 000CF = €9 000S = €8 000n = 5r = 6%
NPV = €
28.NPV & IRRHard
years0123456−150 00025 000+2%+2%+2%+2%+2%r = 8%, NPV = ?

A project costs €150 000 today. Its cash flow is €25 000 at the end of year 1 and grows by 2% per year until the last cash flow at the end of year 6. The cost of capital is 8%. Find the net present value NPV.

C0 = €150 000CF1 = €25 000g = 2%n = 6r = 8%
NPV = €
29.Normal distributionMedium
−3−2−10123zshaded area between −z and z = 0.5705

Drag z so that the shaded area between −z and z under the standard normal curve is 0.5705. Find z to two decimals.

A = 0.5705
z =
30.Normal distributionHard
10 g0X − Y?

The mass X of a product from line 1 and Y from line 2 are independent and normal: X has mean 500 g and standard deviation 8 g, Y has mean 490 g and standard deviation 6 g. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 500 g, σX = 8 gμY = 490 g, σY = 6 g
P =

3Solutions

1.Beam support reactions

Answer: RB = 70 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​ = 50 kNP2​ = 50 kNABRA​RB​3 m1 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.

ΣMA = 0: RB·5 = 50·3 + 50·4
RB = 350/5 = 70 kN
ΣFy = 0: RA = 100 − 70 = 30 kN

Answer

RB = 70 kN
2.Beam support reactions

Answer: RA = 16.64 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 = 6·1.5 = 9 kN, x̄ = (3.5 + 5)/2 = 4.25 m

Equilibrium

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

ΣMA = 0: RB·3.5 = 65·2.5 + 9·4.25
RB = 200.8/3.5 = 57.36 kN
RA = 74 − 57.36 = 16.64 kN

Answer

RA = 16.64 kN
3.Truss: method of joints

Answer: FBC = −38.65 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·4 = 50·3 → Cy = 37.5 kN
ΣFy = 0: Ay = 50 − 37.5 = 12.5 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 = 4/4.123 = 0.9701, cos γ = 1/4.123 = 0.2425
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −37.5/0.9701 = −38.65 kN

Answer

FBC = −38.65 kN (compression)
4.Truss: method of joints

Answer: member CG

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 C

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

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

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

AB: 76.25 kN (T), BC: 77.5 kN (T), CD: 77.5 kN (T), DE: 38.75 kN (T), FG: 76.25 kN (C), GH: 38.75 kN (C), AF: 86.62 kN (C), HE: 54.8 kN (C), BF: 36.25 kN (T), CG: 0, DH: 38.75 kN (T), BG: 1.768 kN (C), DG: 54.8 kN (C)

Answer

Zero-force member: CG
5.Shear force & bending moment

Answer: Vx = −1.5 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 = 3·6 = 18 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 3·6·3
RB = 54/6 = 9 kN
ΣFy = 0: RA = 18 − 9 = 9 kN
w = 3 kN/mABRA​ = 9RB​ = 9section3.5 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.

V = RA − (all downward loads left of the cut)
Vx = 9 − 3·3.5 = −1.5 kN

Answer

Vx = −1.5 kN
6.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 = 57 kN, R2 = 63 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 = 54 kN·m, MC = 42, MD = 24, ME = 0, MF = −30, MG = 0

Answer

Mark B: MB = 54 kN·m
7.Beam deflection

Answer: δ = 2.397 mm

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition).

Consistent units

Work in N and mm: P in N, w in N/mm (kN/m = N/mm), L in mm, E in N/mm² (GPa × 1000), I in mm⁴.

w = 5 N/mm, L = 1500 mm
EI = 1.32 × 10¹² N·mm²

Deflection

δ = wL⁴/(8EI) = 5·1500⁴/(8·1.32 × 10¹²) = 2.397 mm

Answer

δ = 2.397 mm
8.Beam deflection

Answer: hreq = 165.7 mm

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition).

Consistent units

Work in N and mm: P in N, w in N/mm (kN/m = N/mm), L in mm, E in N/mm² (GPa × 1000), I in mm⁴.

w = 2 N/mm, L = 4000 mm, E = 11000 N/mm²

Deflection limit

δallow = L/250 = 4000/250 = 16 mm

Required second moment of area

Ireq = 5wL⁴/(384·E·δallow) = 5·2·4000⁴/(384·11000·16) = 3.788 × 10⁷ mm⁴

Required depth

bh³/12 = Ireq → h = (12·3.788 × 10⁷/100)1/3 = 165.7 mm

Answer

hreq = 165.7 mm

In practice, choose the next standard depth above this value.

9.Column buckling

Answer: Pcr = 107.4 kN

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Smallest second moment of area

A rectangle buckles about its weak axis, using the smaller dimension cubed.

Imin = h·b³/12 = 80·40³/12 = 426667 mm⁴

Effective length

KL = 0.7·4000 = 2800 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·426667/2800² = 107424 N = 107.4 kN

Answer

Pcr = 107.4 kN
10.Column buckling

Answer: σcr = 12.69 MPa

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·60⁴/64 = 636173 mm⁴

Radius of gyration and slenderness

A = 2827 mm²
r = √(I/A) = √(636173/2827) = 15 mm
KL = 0.7·5000 = 3500 mm
KL/r = 3500/15 = 233.3

Critical stress

σcr = π²E/(KL/r)² = π²·70000/233.3² = 12.69 MPa

Answer

σcr = 12.69 MPa
11.Centroid & second moment of area

Answer: Ix = 87.58 × 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 = 280 − 2·10 = 260 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (200·280³ − 190·260³)/12
Ix = 8.758 × 10⁷ mm⁴ = 87.58 × 10⁶ mm⁴

Answer

Ix = 87.58 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σmax = 89.59 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 = 360 − 2·20 = 320 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (120·360³ − 112·320³)/12
Ix = 1.607 × 10⁸ mm⁴

Bending stress

y = 180 mm
σ = M·y/I = 8 × 10⁷·180/1.607 × 10⁸ = 89.59 MPa

Answer

σmax = 89.59 MPa
13.Effective stress in soil

Answer: σ′ = 56.19 kPa

Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).

Total stress

Add the weight of each soil band above X. Above the water table use the dry unit weight, below it the saturated one.

σ = γd·zw + γsat·(z − zw) = 15.5·3 + 19.5·1 = 66 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·1 = 9.81 kPa

Effective stress

σ′ = σ − u = 66 − 9.81 = 56.19 kPa

Answer

σ′ = 56.19 kPa
14.Effective stress in soil

Answer: σ′ = 74.95 kPa

Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).

Total stress

Add the weight of each soil band above X. Above the water table use the dry unit weight, below it the saturated one.

σ = γd·2 + γsat,sand·3 + γsat,clay·2
σ = 16.5·2 + 19·3 + 17·2 = 124 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·5 = 49.05 kPa

Effective stress

σ′ = σ − u = 124 − 49.05 = 74.95 kPa

Answer

σ′ = 74.95 kPa
15.Consolidation settlement

Answer: S = 53.96 mm

Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.

Compare with the preconsolidation pressure

σ′f = 90 + 65 = 155 kPa ≤ 160 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.06·8/(1 + 1.1)·log₁₀(155/90) = 53.96 mm

Answer

S = 53.96 mm
16.Consolidation settlement

Answer: t = 2.078 years

Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.

Drainage path

Hdr = H/2 = 7/2 = 3.5 m

Time

t = Tv·Hdr²/cv = 0.848·3.5²/5 = 2.078 years

Answer

t = 2.078 years
17.Hydrostatic force

Answer: F = 275.9 kN

Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.

Centroid depth and area

yc = d + H/2 = 2.5 + 2.5/2 = 3.75 m
A = H·b = 2.5·3 = 7.5 m²
gated = 2.5 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.75·7.5 = 275.9 kN

Answer

F = 275.9 kN
18.Hydrostatic force

Answer: ycp = 4.188 m

Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.

Centroid depth and area

yc = d + H/2 = 2.5 + 3/2 = 4 m
A = H·b = 3·2 = 6 m²
gated = 2.5 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·4·6 = 296.7 kN

Centre of pressure

Pressure grows with depth, so the resultant acts below the centroid.

Ic = b·H³/12 = 2·3³/12 = 4.5 m⁴
ycp = yc + Ic/(yc·A) = 4 + 4.5/(4·6) = 4.188 m

Answer

ycp = 4.188 m
19.Pipe friction & head loss

Answer: hf = 3.045 m

Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.

Velocity head

V²/(2g) = 0.8²/(2·9.81) = 0.03262 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.028·(500/0.15)·0.8²/(2·9.81) = 3.045 m

Answer

hf = 3.045 m
20.Pipe friction & head loss

Answer: H = 2.206 m

Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.

Velocity

V = Q/A = 0.04/0.03142 = 1.273 m/s
V²/(2g) = 0.08263 m

Loss coefficients

f·L/D = 0.022·200/0.2 = 22
ΣK = 0.5 + 4·0.3 + 2 = 3.7

Energy equation

The outlet jet still carries its velocity head; it is not a loss but it has to be supplied.

H = (1 + 22 + 3.7)·0.08263 = 2.206 m

Answer

H = 2.206 m
21.Open-channel flow (Manning)

Answer: Q = 10 m³/s

Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.

Geometry

A = (b + z·y)·y = (1.5 + 3·1.4)·1.4 = 7.98 m²
P = b + 2y·√(1 + z²) = 1.5 + 2·1.4·√(1 + 3²) = 10.35 m
R = A/P = 0.7707 m

Velocity

V = (1/0.015)·0.77072/3·0.00051/2 = 1.253 m/s

Flow rate

Q = A·V = 7.98·1.253 = 10 m³/s

Answer

Q = 10 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002232 m/m

Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.

Hydraulic radius

R = D/4 = 0.375/4 = 0.09375 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.75/0.2064)² = 0.002232

Answer

S = 0.002232

That is a fall of 2.232 m per kilometre.

23.Pumps & pump power

Answer: Pel = 44.59 kW

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.04·72 = 28.25 kW

Shaft power

Pshaft = 28.25/0.72 = 39.24 kW

Electrical power

Pel = 39.24/0.88 = 44.59 kW

Answer

Pel = 44.59 kW
24.Pumps & pump power

Answer: H = 83.47 m

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Velocity

V = Q/A = 0.02/0.007854 = 2.546 m/s
V²/(2g) = 0.3305 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (100 + 8)·0.3305 = 35.69 m

Pressure head

p/(ρ·g) = 400000/(1000·9.81) = 40.77 m

Pump head

Both surfaces are practically at rest, so there is no velocity head term.

H = Δz + p/(ρ·g) + hL = 7 + 40.77 + 35.69 = 83.47 m

Answer

H = 83.47 m
25.Time value of money

Answer: FV = 40275 €

Time value of money: money today is worth more than the same amount later, because it can earn interest. With interest rate i per period, an amount grows as FV = PV·(1 + i)n. A series of equal payments (an annuity) is valued by adding up each payment, which gives the annuity formulas.

Exponent

r·t = 0.07·10 = 0.7
e0.7 = 2.014

Future value

FV = 20 000·2.014 = €40 275.05

Answer

FV = €40 275.05
26.Time value of money

Answer: FV = 22842 €

Time value of money: money today is worth more than the same amount later, because it can earn interest. With interest rate i per period, an amount grows as FV = PV·(1 + i)n. A series of equal payments (an annuity) is valued by adding up each payment, which gives the annuity formulas.

Monthly rate and number of deposits

i = 0.024/12 = 0.002
N = 12·7 = 84

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 250·(1.183 − 1)/0.002 = €22 842.27

Answer

FV = €22 842.27

You paid in €21 000 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = 3889 €

Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.

Present value of the yearly cash flows

9 000·4.212 = 37 911.27

Present value of the salvage value

8 000/1.338 = 5 978.07

NPV

NPV = −40 000 + 37 911.27 + 5 978.07 = €3 889.34

Answer

NPV = €3 889.34
28.NPV & IRR

Answer: NPV = −29031 €

Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.

Present value of the growing annuity

((1.02)/(1.08))6 = 0.7097
PV = 25 000/(0.08 − 0.02)·(1 − 0.7097) = 120 969.44

NPV

NPV = 120 969.44 − 150 000 = −€29 030.56

Answer

NPV = −€29 030.56

NPV is negative, so the project earns less than the required return.

29.Normal distribution

Answer: z = 0.79

From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.

Area to the left of z

Φ(z) = (1 + 0.5705)/2 = 0.7852

Read the z-table backwards

Find 0.7852 inside the table and read off z.

z = 0.79

Answer

z = 0.79
30.Normal distribution

Answer: P = 0.8413

Sums and differences of normal variables: if X and Y are independent and normal, X + Y and X − Y are normal too. Means add or subtract: E(X ± Y) = μX ± μY. Variances always add, also for a difference: Var(X ± Y) = σX² + σY², so σ = √(σX² + σY²). Standard deviations never add directly. The total of n independent items with the same distribution has mean n·μ and standard deviation σ·√n. Then standardise as usual: z = (x − mean)/σ and read Φ(z).

Distribution of the difference

μ = 500 − 490 = 10 g, σ = 10 g

Standardise

z = (0 − 10)/10 = −1

Probability

P = 1 − Φ(−1) = 0.8413

Answer

P = 0.8413

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