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​ = 10 kNP2​ = 40 kNABRA​RB​ = ?2 m4 m2 m

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

L = 8 mP1 = 10 kN at 2 mP2 = 40 kN at 6 m
RB = kN
2.Beam support reactionsHard
w = 12 kN/mP = 40 kNABCRB​ = ?1.5 m0.5 m0.5 m1.5 m

The beam has a pin at A and a roller at B, 2.5 m from A, and overhangs B to the free end C. It carries a point load P at 2 m from A and a uniformly distributed load w from 1.5 m to the free end at 4 m. Find the vertical reaction RB, taking upward as positive.

AB = 2.5 mAC = 4 mP = 40 kN at 2 mw = 12 kN/m from 1.5 to 4 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB55 kN6 m1 m2 m

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

span = 6 mheight = 2 mB is 1 m from Avertical load = 55 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB35 kN5 kN6 m4 m3 m

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

span = 6 mheight = 3 mB is 4 m from Avertical load = 35 kNhorizontal load = 5 kN ←
FAB = kN
5.Shear force & bending momentMedium
w = 8 kN/mABsection4.5 m0.5 m

Find the bending moment Mx at the section x = 4.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mw = 8 kN/m from 0 to 5 mx = 4.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 3 kN/mP = 30 kNAB1.5 m3.5 m

The simply supported beam carries a uniformly distributed load w over its whole span and a point load P. Find the maximum bending moment Mmax in the beam.

L = 5 mP = 30 kN at 1.5 mw = 3 kN/m from 0 to 5 m
Mmax = kN·m
7.Beam deflectionMedium
P = 15 kNABδ1.5 m0.5 m

A cantilever of length L is fixed at A and carries a point load P at a distance a = 1.5 m from A. Find the deflection δB at the free end B.

P = 15 kNa = 1.5 mL = 2 mE = 200 GPa (steel)I = 23 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
w = 20 kN/mδL = 4 m

A simply supported beam carries a uniformly distributed load w. Its deflection may not exceed span/360. Find the smallest second moment of area Ireq that meets this limit.

w = 20 kN/mL = 4 mE = 200 GPa (steel)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 4 md = 60 mmcross-section

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

L = 4 mE = 70 GPa (aluminium)d = 60 mm
Pcr = kN
10.Column bucklingHard
PL = 3 md = 25 mmcross-section

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

L = 3 mE = 200 GPa (steel)d = 25 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1502001412xdimensions in mm

A symmetric I-section has flanges 150 mm wide and 14 mm thick, an overall depth of 200 mm and a web 12 mm thick. Find its second moment of area Ix about the horizontal centroidal axis x.

B = 150 mmH = 200 mmtf = 14 mmtw = 12 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2601028018xM = 30 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 30 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 260 mmtf = 10 mmtw = 18 mmhw = 280 mmM = 30 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 17 kN/m³γsat​ = 20 kN/m³14 mwater tableXz = 10 m

For the soil profile shown, find the pore water pressure u at point X.

z = 10 mzw = 1 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 20 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 16.5 kN/m³γsat​ = 20 kN/m³4 mclayγsat​ = 17 kN/m³7 mwater tableXz = 7.5 m

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

z = 7.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 20 kN/m³clay: γsat = 17 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 30 kPasandclayCc​ = 0.3, Cr​ = 0.06e0​ = 0.8σ′0​ = 55 kPaOCR = 27 mwater table

A 7 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.06 and e₀ = 0.8. At its mid-depth the effective vertical stress is 55 kPa and the overconsolidation ratio is OCR = 2. A new building adds 30 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7 mCc = 0.3Cr = 0.06e0 = 0.8σ′0 = 55 kPaOCR = 2Δσ = 30 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 4.5 m4.5 msandwater table

In a laboratory oedometer test, a clay specimen 19 mm thick, drained at the top and bottom, reaches 50% consolidation in 4 min. In the field the same clay forms a layer 4.5 m thick. It lies between two sand layers, so water drains out at the top and the bottom. How many days t does the field layer take to reach 50% consolidation?

hlab = 19 mmtlab = 4 minH = 4.5 mfield: double drainage
t = days
17.Hydrostatic forceMedium
gated = 0.5 mH = 1 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 0.5 mH = 1 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 3 mH = 1 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of glycerin, with its top edge 3 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 3 mH = 1 mb = 1.5 mρ = 1260 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
Q = 120 L/sD = 250 mmL = 100 mf = 0.025

Water flows at 120 L/s through a pipe 100 m long with an inside diameter of 250 mm. Use the Darcy friction factor f = 0.025 and g = 9.81 m/s². Find the friction head loss hf.

Q = 120 L/sL = 100 mD = 250 mmf = 0.025g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10Δz = 9 mL = 100 m, D = 100 mm, f = 0.0254× bend (K = 0.3)

Two open reservoirs are joined by a pipe 100 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.025. The water surface of the upper reservoir is 9 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each), a valve (K = 10) 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 = 9 mL = 100 mD = 100 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 1.5 my = 1.1 m1 : 1n = 0.012, S = 0.002

A trapezoidal finished concrete channel has a bottom width of 1.5 m and side slopes of 1:1 (horizontal:vertical). Water flows uniformly 1.1 m deep. Manning n = 0.012 and the bed slope is S = 0.002. Find the flow rate Q in m³/s.

b = 1.5 my = 1.1 mz = 1n = 0.012S = 0.002
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 3.5 my = 1.7 m2 : 1n = 0.025, Q = 15 m³/s

A trapezoidal gravel channel with a bottom width of 3.5 m and side slopes of 2:1 (horizontal:vertical) must carry 15 m³/s in uniform flow at a depth of 1.7 m. Manning n = 0.025. Find the required bed slope S (in m/m).

Q = 15 m³/sb = 3.5 my = 1.7 mz = 2n = 0.025
S = m/m
23.Pumps & pump powerMedium
PQ = 60 L/sH = 38 m

A pump delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 38 m. The pump efficiency is 78% and the electric motor driving it has an efficiency of 94%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 60 L/sH = 38 mηpump = 78%ηmotor = 94%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 20 L/sΔz = 25 mL = 150 m, D = 100 mm, f = 0.022, ΣK = 6

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 25 m higher. The pipe is 150 m long with an inside diameter of 100 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. Find the head H the pump must add.

Q = 20 L/sΔz = 25 mL = 150 mD = 100 mmf = 0.022ΣK = 6
H = m
25.Time value of moneyMedium
years0123…14€5 000FV = ?

You invest €5 000 at 2% per year with continuous compounding. Find the value FV after 14 years.

PV = €5 000r = 2%t = 14
FV = €
26.Time value of moneyHard
months0123…252€150€150€150FV = ?

You save €150 at the end of every month for 21 years. The account pays 4.8% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €1504.8% / 12N = 252
FV = €
27.NPV & IRRMedium
years0123…9−250 00014 000+2%+2%…r = 9%, NPV = ?

A project costs €250 000 today. It generates €14 000 at the end of the first year, and the cash flow then grows by 2% per year forever. The cost of capital is 9%. Find the net present value NPV.

C0 = €250 000CF1 = €14 000g = 2%r = 9%
NPV = €
28.NPV & IRRHard
r (%)NPVABr* = ?0

Project A costs €30 000 and returns €17 500, €12 000, €7 000 at the end of years 1 to 3. Project B costs €40 000 and returns €10 000, €17 500, €23 000. Find the crossover rate r* at which both projects have the same NPV, in percent.

A: −30 000, 17 500, 12 000, 7 000B: −40 000, 10 000, 17 500, 23 000
r* = %
29.Normal distributionMedium
167.85185.35P = ?

The heights of adult men are normally distributed with mean 178 cm and standard deviation 7 cm. What fraction lies between 167.85 and 185.35 cm? Give P as a decimal.

μ = 178σ = 7x1 = 167.85x2 = 185.35
P =
30.Normal distributionHard
μ = 65x = ?95%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Find the value x below which 95% of them lie (the 95th percentile).

μ = 65σ = 10P = 95%
x = points

3Solutions

1.Beam support reactions

Answer: RB = 32.5 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​ = 10 kNP2​ = 40 kNABRA​RB​2 m4 m2 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·8 = 10·2 + 40·6
RB = 260/8 = 32.5 kN
ΣFy = 0: RA = 50 − 32.5 = 17.5 kN

Answer

RB = 32.5 kN
2.Beam support reactions

Answer: RB = 65 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 = 12·2.5 = 30 kN, x̄ = (1.5 + 4)/2 = 2.75 m

Equilibrium

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

ΣMA = 0: RB·2.5 = 40·2 + 30·2.75
RB = 162.5/2.5 = 65 kN
RA = 70 − 65 = 5 kN

Answer

RB = 65 kN
3.Truss: method of joints

Answer: FAB = −51.24 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.

ABBCACACB55 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 55·1 → Cy = 9.167 kN
ΣFy = 0: Ay = 55 − 9.167 = 45.83 kN

Joint A

Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.

sin α = 2/2.236 = 0.8944
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −45.83/0.8944 = −51.24 kN

Answer

FAB = −51.24 kN (compression)
4.Truss: method of joints

Answer: FAB = −23.61 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.

ABBCACACB35 kN5 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 35·4 − 5·3 → Cy = 20.83 kN
ΣFy = 0: Ay = 35 − 20.83 = 14.17 kN
ΣFx = 0: Ax = 5 kN

Joint A

Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.

sin α = 3/5 = 0.6
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −14.17/0.6 = −23.61 kN

Answer

FAB = −23.61 kN (compression)
5.Shear force & bending moment

Answer: Mx = 9 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 = 8·5 = 40 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 8·5·2.5
RB = 100/5 = 20 kN
ΣFy = 0: RA = 40 − 20 = 20 kN
w = 8 kN/mABRA​ = 20RB​ = 20section4.5 m0.5 m

Cut at x = 4.5 m and keep the left part

Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 20·4.5 − 8·4.5·2.25 = 9 kN·m

Answer

Mx = 9 kN·m
6.Shear force & bending moment

Answer: Mmax = 39.38 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.

UDL resultant: W = w·ℓ = 3·5 = 15 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 30·1.5 + 3·5·2.5
RB = 82.5/5 = 16.5 kN
ΣFy = 0: RA = 45 − 16.5 = 28.5 kN

Where is V = 0?

V(1.5⁻) = RA − w·1.5 = 24 kN
V(1.5⁺) = 24 − 30 = −6 kN
The shear changes sign at the load, so the maximum is under the load.

Maximum moment

Mmax = RA·1.5 − w·1.5²/2 = 28.5·1.5 − 3·1.5²/2 = 39.38 kN·m

Answer

Mmax = 39.38 kN·m

It occurs at x = 1.5 m from A.

7.Beam deflection

Answer: δB = 5.503 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 = 15000 N, a = 1500 mm, L = 2000 mm
EI = 4.6 × 10¹² N·mm²

Deflection at the free end

Deflection at the load plus the slope at the load times the remaining length.

δP = Pa³/(3EI) = 3.668 mm
θP = Pa²/(2EI) = 0.003668 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 5.503 mm

Answer

δB = 5.503 mm
8.Beam deflection

Answer: Ireq = 30 × 10⁶ mm⁴

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).

Deflection limit

δallow = L/360 = 4000/360 = 11.11 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·20·4000⁴/(384·200000·11.11) = 3 × 10⁷ mm⁴
Ireq = 30 × 10⁶ mm⁴

Answer

Ireq = 30 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 27.47 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 round section has the same I about every axis.

I = πd⁴/64 = π·60⁴/64 = 636173 mm⁴

Effective length

KL = 1·4000 = 4000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·636173/4000² = 27470 N = 27.47 kN

Answer

Pcr = 27.47 kN
10.Column buckling

Answer: σcr = 17.48 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·25⁴/64 = 19175 mm⁴

Radius of gyration and slenderness

A = 490.9 mm²
r = √(I/A) = √(19175/490.9) = 6.25 mm
KL = 0.7·3000 = 2100 mm
KL/r = 2100/6.25 = 336

Critical stress

σcr = π²E/(KL/r)² = π²·200000/336² = 17.48 MPa

Answer

σcr = 17.48 MPa
11.Centroid & second moment of area

Answer: Ix = 41.48 × 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 = 200 − 2·14 = 172 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (150·200³ − 138·172³)/12
Ix = 4.148 × 10⁷ mm⁴ = 41.48 × 10⁶ mm⁴

Answer

Ix = 41.48 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 43.76 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 = 260·10 = 2600 mm², yf = 280 + 10/2 = 285 mm
web: Aw = 18·280 = 5040 mm², yw = 280/2 = 140 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2600·285 + 5040·140)/7640 = 189.3 mm

Parallel-axis theorem

flange: 260·10³/12 + 2600·(285 − 189.3)² = 2.381 × 10⁷ mm⁴
web: 18·280³/12 + 5040·(140 − 189.3)² = 4.52 × 10⁷ mm⁴
Ix = 2.381 × 10⁷ + 4.52 × 10⁷ = 6.901 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 290 − 189.3 = 100.7 mm
σ = M·y/I = 3 × 10⁷·100.7/6.901 × 10⁷ = 43.76 MPa

Answer

σtop = 43.76 MPa
13.Effective stress in soil

Answer: u = 88.29 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).

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·9 = 88.29 kPa

Answer

u = 88.29 kPa
14.Effective stress in soil

Answer: σ = 136 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·1 + γsat,sand·3 + γsat,clay·3.5
σ = 16.5·1 + 20·3 + 17·3.5 = 136 kPa

Answer

σ = 136 kPa
15.Consolidation settlement

Answer: S = 44.11 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.

Preconsolidation pressure

σ′p = OCR·σ′0 = 2·55 = 110 kPa

Compare with the preconsolidation pressure

σ′f = 55 + 30 = 85 kPa ≤ 110 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.06·7/(1 + 0.8)·log₁₀(85/55) = 44.11 mm

Answer

S = 44.11 mm
16.Consolidation settlement

Answer: t = 155.8 days

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 paths

Hdr,lab = 19/2 = 9.5 mm = 0.0095 m
Hdr,field = 4.5/2 = 2.25 m

Scale the time

t = Tv·Hdr²/cv with the same T_v and cv in the lab and the field.

tfield = 4·(2.25/0.0095)² = 224377 min
tfield = 224377/1440 = 155.8 days

Answer

t = 155.8 days
17.Hydrostatic force

Answer: F = 19.62 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 = 0.5 + 1/2 = 1 m
A = H·b = 1·2 = 2 m²
gated = 0.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·1·2 = 19.62 kN

Answer

F = 19.62 kN
18.Hydrostatic force

Answer: ycp = 3.524 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 = 3 + 1/2 = 3.5 m
A = H·b = 1·1.5 = 1.5 m²
gated = 3 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·3.5·1.5 = 64.89 kN

Centre of pressure

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

Ic = b·H³/12 = 1.5·1³/12 = 0.125 m⁴
ycp = yc + Ic/(yc·A) = 3.5 + 0.125/(3.5·1.5) = 3.524 m

Answer

ycp = 3.524 m
19.Pipe friction & head loss

Answer: hf = 3.046 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.

Mean velocity

A = π·0.25²/4 = 0.04909 m²
V = Q/A = 0.12/0.04909 = 2.445 m/s

Velocity head

V²/(2g) = 2.445²/(2·9.81) = 0.3046 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.025·(100/0.25)·2.445²/(2·9.81) = 3.046 m

Answer

hf = 3.046 m
20.Pipe friction & head loss

Answer: Q = 17 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 = 0.025·100/0.1 = 25
ΣK = 0.5 + 4·0.3 + 10 + 1.0 = 12.7

Energy equation

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

9 = (25 + 12.7)·V²/(2·9.81)
V = √(2·9.81·9/37.7) = 2.164 m/s

Flow rate

Q = V·π·D²/4 = 2.164·0.007854 = 0.017 m³/s = 17 L/s

Answer

Q = 17 L/s
21.Open-channel flow (Manning)

Answer: Q = 7.752 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 + 1·1.1)·1.1 = 2.86 m²
P = b + 2y·√(1 + z²) = 1.5 + 2·1.1·√(1 + 1²) = 4.611 m
R = A/P = 0.6202 m

Velocity

V = (1/0.012)·0.62022/3·0.0021/2 = 2.71 m/s

Flow rate

Q = A·V = 2.86·2.71 = 7.752 m³/s

Answer

Q = 7.752 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0009498 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.

Geometry

A = (b + z·y)·y = (3.5 + 2·1.7)·1.7 = 11.73 m²
P = b + 2y·√(1 + z²) = 3.5 + 2·1.7·√(1 + 2²) = 11.1 m
R = A/P = 1.057 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.025·15/(11.73·1.037) = 0.03082
S = 0.03082² = 0.0009498

Answer

S = 0.0009498

That is a fall of 0.9498 m per kilometre.

23.Pumps & pump power

Answer: Pel = 30.51 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 = 1000·9.81·0.06·38 = 22.37 kW

Shaft power

Pshaft = 22.37/0.78 = 28.68 kW

Electrical power

Pel = 28.68/0.94 = 30.51 kW

Answer

Pel = 30.51 kW
24.Pumps & pump power

Answer: H = 37.89 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) = (33 + 6)·0.3305 = 12.89 m

Pump head

Both surfaces are open and practically at rest, so pressure and velocity terms drop out.

H = Δz + hL = 25 + 12.89 = 37.89 m

Answer

H = 37.89 m
25.Time value of money

Answer: FV = 6616 €

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 = 0.02·14 = 0.28
e0.28 = 1.323

Future value

FV = 5 000·1.323 = €6 615.65

Answer

FV = €6 615.65
26.Time value of money

Answer: FV = 65048 €

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 = 0.048/12 = 0.004
N = 12·21 = 252

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 150·(2.735 − 1)/0.004 = €65 047.93

Answer

FV = €65 047.93

You paid in €37 800 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −50000 €

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.

Value of the cash flows

PV = 14 000/(0.09 − 0.02) = 200 000.00

NPV

NPV = 200 000.00 − 250 000 = −€50 000.00

Answer

NPV = −€50 000.00

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

28.NPV & IRR

Answer: r* = 9.287 %

Crossover rate: the discount rate at which two projects have the same NPV. It is the IRR of the difference in their cash flows (B − A). Below it the project with the later, larger cash flows has the higher NPV; above it the other one wins.

Difference in cash flows

ΔCF0 = −40 000 − (−30 000) = −10 000
ΔCF1 = 10 000 − 17 500 = −7 500
ΔCF2 = 17 500 − 12 000 = 5 500
ΔCF3 = 23 000 − 7 000 = 16 000

IRR of the difference

NPVΔ(9%) = 103.44
NPVΔ(10%) = −251.69
r* = 9.287%

Answer

r* = 9.287%

Check: at 9.287% both NPVs are €1 422.68.

29.Normal distribution

Answer: P = 0.7796

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 = (167.85 − 178)/7 = −1.45
z₂ = (185.35 − 178)/7 = 1.05

Area between

P = Φ(1.05) − Φ(−1.45) = 0.8531 − 0.07353 = 0.7796

Answer

P = 0.7796
30.Normal distribution

Answer: x = 81.45 points

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 for the percentile

Φ(z) = 0.95 → z = 1.645

Back to x

x = 65 + 1.645·10 = 81.45 points

Answer

x = 81.45 points

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