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​ = 30 kNP2​ = 20 kNABRA​ = ?RB​1 m5 m4 m

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

L = 10 mP1 = 30 kN at 1 mP2 = 20 kN at 6 m
RA = kN
2.Beam support reactionsHard
w = 3 kN/mP = 50 kNABCRA​ = ?2.5 m1.5 m0.5 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 2.5 m from A and a uniformly distributed load w from 4 m to the free end at 6 m. Find the vertical reaction RA, taking upward as positive.

AB = 4.5 mAC = 6 mP = 50 kN at 2.5 mw = 3 kN/m from 4 to 6 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB40 kN8 m3 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 3 m from Avertical load = 40 kN
FAC = kN
4.Truss: method of jointsHard
ABCDEFGH35 kN35 kN35 kN35 kN4 × 4 m3 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 ↓D: 35 kN ↓F: 35 kN ↓F: 35 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
5.Shear force & bending momentMedium
P1​ = 80 kNP2​ = 50 kNAB5 m1 m2 m

The simply supported beam carries two point loads. Find the maximum bending moment Mmax in the beam.

L = 8 mP1 = 80 kN at 5 mP2 = 50 kN at 6 m
Mmax = kN·m
6.Shear force & bending momentHard
w = 12 kN/mABC5 m1 m

The beam rests on a pin at A and a roller at B and overhangs B by 1 m to the free end C. A uniformly distributed load w acts over the whole length A–C. Find the distance xc from A to the point of contraflexure between the supports (where the bending moment changes sign).

L = 6 mw = 12 kN/m from 0 to 6 msupports at x = 0 and x = 5 m
xc = m
7.Beam deflectionMedium
w = 8 kN/mδL = 4 m

A simply supported beam carries a uniformly distributed load w over its whole span. Find the maximum deflection δmax, at midspan.

w = 8 kN/mL = 4 mE = 70 GPa (aluminium)I = 57 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 4 kN/mP = 28 kNδL = 8 m

A simply supported beam carries a uniformly distributed load w and a point load P at midspan. Using superposition, find the midspan deflection δmax.

P = 28 kNw = 4 kN/mL = 8 mE = 200 GPa (steel)I = 120 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 1 m30 × 100 mmcross-section

A column of length L made of steel is pinned at both ends. Using Euler’s formula, find its critical buckling load Pcr.

L = 1 mE = 200 GPa (steel)b × h = 30 × 100 mm
Pcr = kN
10.Column bucklingHard
PL = 2.5 md = 40 mmcross-section

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

L = 2.5 mE = 200 GPa (steel)d = 40 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1201520012xdimensions in mm

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

bf = 120 mmtf = 15 mmtw = 12 mmhw = 200 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1201528016xM = 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 = 120 mmtf = 15 mmtw = 16 mmhw = 280 mmM = 20 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 19.5 kN/m³10 mwater tableXz = 9 m

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

z = 9 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19.5 kN/m³
σ = kPa
14.Effective stress in soilHard
sandγd​ = 17 kN/m³γsat​ = 19 kN/m³3 mclayγsat​ = 17.5 kN/m³5 mwater tableXz = 5.5 m

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

z = 5.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 19 kN/m³clay: γsat = 17.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 230 kPasandclayCc​ = 0.25, Cr​ = 0.05e0​ = 0.9σ′0​ = 50 kPaσ′p​ = 170 kPa7.5 mwater table

A 7.5 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.05 and e₀ = 0.9. At its mid-depth the effective vertical stress is 50 kPa and the preconsolidation pressure is 170 kPa. A new building adds 230 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7.5 mCc = 0.25Cr = 0.05e0 = 0.9σ′0 = 50 kPaσ′p = 170 kPaΔσ = 230 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 3 mcv​ = 4 m²/year3 msandwater table

A clay layer 3 m thick has a coefficient of consolidation cv = 4 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 70% average consolidation the time factor is Tv = 0.403. How many years t does the layer take to reach 70% consolidation?

H = 3 mcv = 4 m²/yearU = 70%Tv = 0.403double drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 1.5 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 1.5 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2.5 mH = 1.5 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of water, 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 = 1.5 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 1.9 m/sD = 100 mmL = 400 mf = 0.02

Water (ρ = 1000 kg/m³) flows at 1.9 m/s through a horizontal pipe, 400 m long, with an inside diameter of 100 mm. Use the Darcy friction factor f = 0.02 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1.9 m/sL = 400 mD = 100 mmf = 0.02ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 5Δz = 11 mL = 400 m, D = 300 mm, f = 0.0153× bend (K = 0.3)

Two open reservoirs are joined by a pipe 400 m long with an inside diameter of 300 mm and a Darcy friction factor f = 0.015. The water surface of the upper reservoir is 11 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each), a valve (K = 5) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². Find the flow rate Q in L/s.

Δz = 11 mL = 400 mD = 300 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 5.5 my = 2 m2 : 1n = 0.022, S = 0.0015

A trapezoidal clean earth channel has a bottom width of 5.5 m and side slopes of 2:1 (horizontal:vertical). Water flows uniformly 2 m deep. Manning n = 0.022 and the bed slope is S = 0.0015. Find the flow rate Q in m³/s.

b = 5.5 my = 2 mz = 2n = 0.022S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 200 mmn = 0.013, V = 0.9 m/s

A concrete sewer with an inside diameter of 200 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.9 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 200 mmn = 0.013V = 0.9 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 10 L/sH = 20 m

A pump delivers 10 L/s of water (ρ = 1000 kg/m³) against a head of 20 m. The pump efficiency is 70% and the electric motor driving it has an efficiency of 92%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 10 L/sH = 20 mηpump = 70%ηmotor = 92%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 100 L/sΔz = 15 mL = 100 m, D = 250 mm, f = 0.022, ΣK = 6

A pump moves 100 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 15 m higher. The pipe is 100 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 75%. Find the shaft power Pshaft in kW.

Q = 100 L/sΔz = 15 mL = 100 mD = 250 mmf = 0.022ΣK = 6η = 75%
Pshaft = kW
25.Time value of moneyMedium
years01234567PV = ?€20 000

You need €20 000 in 7 years. An account pays 6% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €20 0006% / 12n = 7
PV = €
26.Time value of moneyHard
months0123…348€150€150€150FV = ?

You save €150 at the end of every month for 29 years. The account pays 6% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €1506% / 12N = 348
FV = €
27.NPV & IRRMedium
years0123−60 00030 00020 00023 000

An investment of €60 000 gives these cash flows at the end of years 1 to 3: €30 000, €20 000, €23 000. The cost of capital is 12%. Find the net present value NPV.

r = 12%CF0 = −60 000CF1 = 30 000CF2 = 20 000CF3 = 23 000
NPV = €
28.NPV & IRRHard
years012−40 00027 50029 000

A project costs €40 000 and returns €27 500, €29 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 27 500CF2 = 29 000
IRR = %
29.Normal distributionMedium
245.25251P = ?

The bag weights are normally distributed with mean 250 g and standard deviation 5 g. What fraction lies between 245.25 and 251 g? Give P as a decimal.

μ = 250σ = 5x1 = 245.25x2 = 251
P =
30.Normal distributionHard
0.03 mm0D − d?

Hole diameters D are normal with mean 25.03 mm and standard deviation 0.01 mm. Shaft diameters d are independent and normal with mean 25 mm and standard deviation 0.02 mm. A randomly chosen shaft fits when D − d > 0. Find the probability P that it fits. Round z to two decimals.

hole: μ = 25.03 mm, σ = 0.01 mmshaft: μ = 25 mm, σ = 0.02 mm
P =

3Solutions

1.Beam support reactions

Answer: RA = 35 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​ = 30 kNP2​ = 20 kNABRA​RB​1 m5 m4 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·10 = 30·1 + 20·6
RB = 150/10 = 15 kN
ΣFy = 0: RA = 50 − 15 = 35 kN

Answer

RA = 35 kN
2.Beam support reactions

Answer: RA = 21.56 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 = 3·2 = 6 kN, x̄ = (4 + 6)/2 = 5 m

Equilibrium

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

ΣMA = 0: RB·4.5 = 50·2.5 + 6·5
RB = 155/4.5 = 34.44 kN
RA = 56 − 34.44 = 21.56 kN

Answer

RA = 21.56 kN
3.Truss: method of joints

Answer: FAC = 25 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.

ABBCACACB40 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 40·3 → Cy = 15 kN
ΣFy = 0: Ay = 40 − 15 = 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 = 3/5.831 = 0.5145, cos γ = 5/5.831 = 0.8575
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −15/0.5145 = −29.15 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−29.15)·0.8575 = 25 kN

Answer

FAC = 25 kN (tension)
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 G

FG and GH 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: 107.9 kN (T), BC: 107.9 kN (T), CD: 67.08 kN (T), DE: 67.08 kN (T), FG: 87.5 kN (C), GH: 87.5 kN (C), AF: 91.15 kN (C), HE: 83.85 kN (C), BF: 35 kN (T), CG: 0, DH: 35 kN (T), FC: 25.52 kN (C), HC: 25.52 kN (T)

Answer

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

Answer: Mmax = 212.5 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. Maximum moment: since dM/dx = V, the bending moment has its peak where the shear force passes through zero, either at a point load or inside a distributed load.

Support reactions

Equilibrium of the whole beam.

ΣMA = 0: RB·8 = 80·5 + 50·6
RB = 700/8 = 87.5 kN
ΣFy = 0: RA = 130 − 87.5 = 42.5 kN

Moment under each load

Keep the part left of each load.

under P1: M = RA·5 = 42.5·5 = 212.5 kN·m
under P2: M = RB·2 = 87.5·2 = 175 kN·m

Largest value

Mmax = 212.5 kN·m (under P1)

Answer

Mmax = 212.5 kN·m
6.Shear force & bending moment

Answer: xc = 4.8 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. Maximum moment: since dM/dx = V, the bending moment has its peak where the shear force passes through zero, either at a point load or inside a distributed load.

Support reactions

Equilibrium of the whole beam, including the load on the overhang.

UDL resultant: W = w·ℓ = 12·6 = 72 kN, acting at x̄ = 3 m
ΣMA = 0: RB·5 = 12·6·3
RB = 216/5 = 43.2 kN
ΣFy = 0: RA = 72 − 43.2 = 28.8 kN

Zero moment

Between the supports M(x) = RA·x − w·x²/2. Apart from x = 0 it is zero at x = 2RA/w.

RA·xc − w·xc²/2 = 0
xc = 2·28.8/12 = 4.8 m

Answer

xc = 4.8 m
7.Beam deflection

Answer: δmax = 6.683 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 = 8 N/mm, L = 4000 mm
EI = 3.99 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·8·4000⁴/(384·3.99 × 10¹²) = 6.683 mm

Answer

δmax = 6.683 mm
8.Beam deflection

Answer: δmax = 21.33 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.

P = 28000 N, w = 4 N/mm, L = 8000 mm, EI = 2.4 × 10¹³ N·mm²

Each load on its own

δP = PL³/(48EI) = 28000·8000³/(48·2.4 × 10¹³) = 12.44 mm
δw = 5wL⁴/(384EI) = 5·4·8000⁴/(384·2.4 × 10¹³) = 8.889 mm

Add them

δmax = 12.44 + 8.889 = 21.33 mm

Answer

δmax = 21.33 mm
9.Column buckling

Answer: Pcr = 444.1 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 = 100·30³/12 = 225000 mm⁴

Effective length

KL = 1·1000 = 1000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·225000/1000² = 444132 N = 444.1 kN

Answer

Pcr = 444.1 kN
10.Column buckling

Answer: σcr = 7.896 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·40⁴/64 = 125664 mm⁴

Radius of gyration and slenderness

A = 1257 mm²
r = √(I/A) = √(125664/1257) = 10 mm
KL = 2·2500 = 5000 mm
KL/r = 5000/10 = 500

Critical stress

σcr = π²E/(KL/r)² = π²·200000/500² = 7.896 MPa

Answer

σcr = 7.896 MPa
11.Centroid & second moment of area

Answer: Ix = 19.92 × 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 = 120·15 = 1800 mm², yf = 200 + 15/2 = 207.5 mm
web: Aw = 12·200 = 2400 mm², yw = 200/2 = 100 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (1800·207.5 + 2400·100)/4200 = 146.1 mm

Parallel-axis theorem

flange: 120·15³/12 + 1800·(207.5 − 146.1)² = 6.826 × 10⁶ mm⁴
web: 12·200³/12 + 2400·(100 − 146.1)² = 1.309 × 10⁷ mm⁴
Ix = 6.826 × 10⁶ + 1.309 × 10⁷ = 1.992 × 10⁷ mm⁴ = 19.92 × 10⁶ mm⁴

Answer

Ix = 19.92 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σbottom = 63.69 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 = 120·15 = 1800 mm², yf = 280 + 15/2 = 287.5 mm
web: Aw = 16·280 = 4480 mm², yw = 280/2 = 140 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (1800·287.5 + 4480·140)/6280 = 182.3 mm

Parallel-axis theorem

flange: 120·15³/12 + 1800·(287.5 − 182.3)² = 1.996 × 10⁷ mm⁴
web: 16·280³/12 + 4480·(140 − 182.3)² = 3.728 × 10⁷ mm⁴
Ix = 1.996 × 10⁷ + 3.728 × 10⁷ = 5.724 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 182.3 mm
σ = M·y/I = 2 × 10⁷·182.3/5.724 × 10⁷ = 63.69 MPa

Answer

σbottom = 63.69 MPa
13.Effective stress in soil

Answer: σ = 165 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) = 16·3 + 19.5·6 = 165 kPa

Answer

σ = 165 kPa
14.Effective stress in soil

Answer: σ′ = 62.41 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·1 + γsat,clay·2.5
σ = 17·2 + 19·1 + 17.5·2.5 = 96.75 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·3.5 = 34.34 kPa

Effective stress

σ′ = σ − u = 96.75 − 34.34 = 62.41 kPa

Answer

σ′ = 62.41 kPa
15.Consolidation settlement

Answer: S = 318.8 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 = 50 + 230 = 280 kPa > 170 kPa

Settlement

Recompression up to σ′p, virgin compression beyond it.

S = 0.05·7.5/(1 + 0.9)·log₁₀(170/50) + 0.25·7.5/(1 + 0.9)·log₁₀(280/170)
S = 104.9 + 213.9 = 318.8 mm

Answer

S = 318.8 mm
16.Consolidation settlement

Answer: t = 0.2267 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 = 3/2 = 1.5 m

Time

t = Tv·Hdr²/cv = 0.403·1.5²/4 = 0.2267 years

Answer

t = 0.2267 years
17.Hydrostatic force

Answer: F = 121.4 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 + 1.5/2 = 2.75 m
A = H·b = 1.5·3 = 4.5 m²
gated = 2 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.75·4.5 = 121.4 kN

Answer

F = 121.4 kN
18.Hydrostatic force

Answer: ycp = 3.308 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 + 1.5/2 = 3.25 m
A = H·b = 1.5·1 = 1.5 m²
gated = 2.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.25·1.5 = 47.82 kN

Centre of pressure

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

Ic = b·H³/12 = 1·1.5³/12 = 0.2813 m⁴
ycp = yc + Ic/(yc·A) = 3.25 + 0.2813/(3.25·1.5) = 3.308 m

Answer

ycp = 3.308 m
19.Pipe friction & head loss

Answer: Δp = 144.4 kPa

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.

Head loss

hf = f·(L/D)·V²/(2g) = 0.02·(400/0.1)·1.9²/(2·9.81) = 14.72 m

Pressure drop

The pipe is horizontal and the velocity does not change, so the energy equation reduces to Δp = ρ·g·hf.

Δp = ρ·g·hf = 1000·9.81·14.72 = 144400 Pa = 144.4 kPa

Answer

Δp = 144.4 kPa
20.Pipe friction & head loss

Answer: Q = 198.4 L/s

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.

Loss coefficients

f·L/D = 0.015·400/0.3 = 20
ΣK = 0.5 + 3·0.3 + 5 + 1.0 = 7.4

Energy equation

Both surfaces are open to the air and practically at rest, so all of Δz is lost in the pipe.

11 = (20 + 7.4)·V²/(2·9.81)
V = √(2·9.81·11/27.4) = 2.807 m/s

Flow rate

Q = V·π·D²/4 = 2.807·0.07069 = 0.1984 m³/s = 198.4 L/s

Answer

Q = 198.4 L/s
21.Open-channel flow (Manning)

Answer: Q = 40.16 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 = (5.5 + 2·2)·2 = 19 m²
P = b + 2y·√(1 + z²) = 5.5 + 2·2·√(1 + 2²) = 14.44 m
R = A/P = 1.315 m

Velocity

V = (1/0.022)·1.3152/3·0.00151/2 = 2.113 m/s

Flow rate

Q = A·V = 19·2.113 = 40.16 m³/s

Answer

Q = 40.16 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.007432 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 = 0.2/4 = 0.05 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.9/0.1357)² = 0.007432

Answer

S = 0.007432

That is a fall of 7.432 m per kilometre.

23.Pumps & pump power

Answer: Pel = 3.047 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 = 1000·9.81·0.01·20 = 1.962 kW

Shaft power

Pshaft = 1.962/0.7 = 2.803 kW

Electrical power

Pel = 2.803/0.92 = 3.047 kW

Answer

Pel = 3.047 kW
24.Pumps & pump power

Answer: Pshaft = 23.71 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.

Velocity

V = Q/A = 0.1/0.04909 = 2.037 m/s
V²/(2g) = 0.2115 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (8.8 + 6)·0.2115 = 3.131 m

Pump head

H = Δz + hL = 15 + 3.131 = 18.13 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.1·18.13/0.75 = 23.71 kW

Answer

Pshaft = 23.71 kW
25.Time value of money

Answer: PV = 13155 €

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.

Rate and number of periods

i = 0.06/12 = 0.005
N = 12·7 = 84

Present value

PV = FV/(1 + i)N = 20 000/1.52 = €13 154.70

Answer

PV = €13 154.70
26.Time value of money

Answer: FV = 140181 €

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 = 0.06/12 = 0.005
N = 12·29 = 348

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 150·(5.673 − 1)/0.005 = €140 180.87

Answer

FV = €140 180.87

You paid in €52 200 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −899.5 €

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 each cash flow

CF0 = −60 000
CF1/(1 + 0.12)1 = 30 000/1.12 = 26 785.71
CF2/(1 + 0.12)2 = 20 000/1.254 = 15 943.88
CF3/(1 + 0.12)3 = 23 000/1.405 = 16 370.95

Add them up

NPV = €−899.46

Answer

NPV = €−899.46

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

28.NPV & IRR

Answer: IRR = 26.2 %

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.

Bracket the IRR

NPV falls as the rate rises, so the IRR lies between a rate with positive NPV and one with negative NPV.

NPV(25%) = 560.00
NPV(30%) = −1 686.39

Narrow down

Linear interpolation gives a first estimate; repeating it (or a calculator's IRR function) gives the exact rate.

IRR ≈ 25 + 5·560.00/(560.00 − (−1 686.39)) = 26.25%
exact: NPV(26.2%) = 0 → IRR = 26.2%

Answer

IRR = 26.2%
29.Normal distribution

Answer: P = 0.4082

Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.

z-scores

z₁ = (245.25 − 250)/5 = −0.95
z₂ = (251 − 250)/5 = 0.2

Area between

P = Φ(0.2) − Φ(−0.95) = 0.5793 − 0.1711 = 0.4082

Answer

P = 0.4082
30.Normal distribution

Answer: P = 0.9099

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 = 25.03 − 25 = 0.03 mm, σ = 0.02236 mm

Standardise

z = (0 − 0.03)/0.02236 = −1.34

Probability

P = 1 − Φ(−1.34) = 0.9099

Answer

P = 0.9099

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