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​ = 45 kNP2​ = 10 kNABRA​ = ?RB​1 m3 m6 m

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

L = 10 mP1 = 45 kN at 1 mP2 = 10 kN at 4 m
RA = kN
2.Beam support reactionsHard
w = 12 kN/mP = 75 kNABCRB​ = ?3 m2 m3 m

The beam has a pin at A and a roller at B, 5 m from A, and overhangs B to the free end C. It carries a point load P at 3 m from A and a uniformly distributed load w from 5 m to the free end at 8 m. Find the vertical reaction RB, taking upward as positive.

AB = 5 mAC = 8 mP = 75 kN at 3 mw = 12 kN/m from 5 to 8 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB25 kN8 m3 m4 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 = 4 mB is 3 m from Avertical load = 25 kN
FAC = kN
4.Truss: method of jointsHard
ABBCACACB60 kN10 kN6 m5 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 5 m from Avertical load = 60 kNhorizontal load = 10 kN →
FAB = kN
5.Shear force & bending momentMedium
w = 5 kN/mABsection3.5 m1.5 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 = 5 mw = 5 kN/m from 0 to 5 mx = 3.5 m
Vx = kN
6.Shear force & bending momentHard
15 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.

15 kN @ 6 m60 kN @ 3 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 = 12 kN/mδL = 2 m

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

w = 12 kN/mL = 2 mE = 11 GPa (timber)I = 8.5 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 20 kN/mδL = 5 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 = 5 mE = 70 GPa (aluminium)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 1.5 md = 40 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 = 1.5 mE = 70 GPa (aluminium)d = 40 mm
Pcr = kN
10.Column bucklingHard
P = 130 kNL = 4 md = ?cross-section

A solid round column of length L made of steel is fixed at both ends. It must carry 130 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 130 kNn = 2.5L = 4 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
B = 120H = 400t = 6xdimensions in mm

A hollow rectangular (box) section has outer width B = 120 mm, outer height H = 400 mm and a uniform wall thickness t = 6 mm. Find its radius of gyration r about the horizontal centroidal axis.

B = 120 mmH = 400 mmt = 6 mm
r = mm
12.Centroid & second moment of areaHard
1401014014xM = 15 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 15 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 140 mmtf = 10 mmtw = 14 mmhw = 140 mmM = 15 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 19.5 kN/m³14 mwater tableXz = 8 m

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

z = 8 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 20.5 kN/m³3 mclayγsat​ = 17.5 kN/m³7 mwater tableXz = 6.5 m

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

z = 6.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 17.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 50 kPasandclayCc​ = 0.5, Cr​ = 0.06e0​ = 1.2σ′0​ = 55 kPaσ′p​ = 85 kPa7.5 mwater table

A 7.5 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.06 and e₀ = 1.2. At its mid-depth the effective vertical stress is 55 kPa and the preconsolidation pressure is 85 kPa. A new building adds 50 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7.5 mCc = 0.5Cr = 0.06e0 = 1.2σ′0 = 55 kPaσ′p = 85 kPaΔσ = 50 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 6.5 mcv​ = 2.5 m²/year6.5 msandwater table

A clay layer 6.5 m thick has a coefficient of consolidation cv = 2.5 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 = 6.5 mcv = 2.5 m²/yearU = 70%Tv = 0.403double drainage
t = years
17.Hydrostatic forceMedium
gated = 0.5 mH = 1.5 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of water, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 0.5 mH = 1.5 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2.5 mH = 3 m

A vertical rectangular gate 1.5 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 = 1.5 mρ = 1260 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
Q = 5 L/sD = 75 mmL = 300 mf = 0.025

Water flows at 5 L/s through a pipe 300 m long with an inside diameter of 75 mm. Use the Darcy friction factor f = 0.025 and g = 9.81 m/s². Find the friction head loss hf.

Q = 5 L/sL = 300 mD = 75 mmf = 0.025g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5Δz = ?L = 300 m, D = 250 mm, f = 0.023× bend (K = 0.3)

Two open reservoirs are joined by a pipe 300 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.02. 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. What difference in water level Δz between the reservoirs gives a flow rate of 75 L/s?

Q = 75 L/sL = 300 mD = 250 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
D = 900 mmn = 0.013, S = 0.004

A concrete storm sewer with an inside diameter of 900 mm flows half full. Manning n = 0.013 and the slope is S = 0.004. Find the flow rate Q in m³/s.

D = 900 mmn = 0.013S = 0.004
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2 my = 0.5 mn = 0.014, Q = 2.4 m³/s

A rectangular unfinished concrete channel 2 m wide must carry 2.4 m³/s in uniform flow at a depth of 0.5 m. Manning n = 0.014. Find the required bed slope S (in m/m).

Q = 2.4 m³/sb = 2 my = 0.5 mn = 0.014
S = m/m
23.Pumps & pump powerMedium
PQ = 80 L/sH = 70 m

A pump with an efficiency of 75% delivers 80 L/s of water (ρ = 1000 kg/m³) against a head of 70 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 80 L/sH = 70 mη = 75%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
200 kPa (gauge)PQ = 120 L/sΔz = 17 mL = 100 m, D = 250 mm, f = 0.018, ΣK = 6

A pump moves 120 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 17 m higher. The pipe is 100 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 6 (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 200 kPa. Find the head H the pump must add.

Q = 120 L/sΔz = 17 mL = 100 mD = 250 mmf = 0.018ΣK = 6ptank = 200 kPa
H = m
25.Time value of moneyMedium
years0123456PV = ?€10 000

You need €10 000 in 6 years. An account pays 5% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €10 0005% / 12n = 6
PV = €
26.Time value of moneyHard
months01…96…300€300 000AB = ?A4.2% / 12

A mortgage of €300 000 is repaid with equal monthly payments over 25 years at 4.2% per year, compounded monthly. How much is still owed just after the payment at the end of year 8? Find the outstanding balance B.

P = €300 0004.2% / 12N = 300k = 96
B = €
27.NPV & IRRMedium
years0123456−20 0006 5006 5006 5006 5006 5006 500

A project costs €20 000 today and returns €6 500 at the end of each year for 6 years. The cost of capital is 5%. Assume cash flows arrive evenly through each year. Find the discounted payback period DPB in years.

r = 5%CF0 = −20 000CF1 = 6 500CF2 = 6 500CF3 = 6 500CF4 = 6 500CF5 = 6 500CF6 = 6 500
DPB = years
28.NPV & IRRHard
years0123−20 00011 50012 50014 000

A project costs €20 000 and returns €11 500, €12 500, €14 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −20 000CF1 = 11 500CF2 = 12 500CF3 = 14 000
IRR = %
29.Normal distributionMedium
32 min35.8 minX + Y?

X is normal with mean 12 min and standard deviation 1.5 min; Y is independent and normal with mean 20 min and standard deviation 2 min. Find the probability P that X + Y is more than 35.8 min. Round z to two decimals.

μX = 12, σX = 1.5μY = 20, σY = 2X + Y > 35.8 min
P =
30.Normal distributionHard
μ = 65x = ?5%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Find the value x below which 5% of them lie (the 5th percentile).

μ = 65σ = 10P = 5%
x = points

3Solutions

1.Beam support reactions

Answer: RA = 46.5 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​ = 45 kNP2​ = 10 kNABRA​RB​1 m3 m6 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 = 45·1 + 10·4
RB = 85/10 = 8.5 kN
ΣFy = 0: RA = 55 − 8.5 = 46.5 kN

Answer

RA = 46.5 kN
2.Beam support reactions

Answer: RB = 91.8 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 = 12·3 = 36 kN, x̄ = (5 + 8)/2 = 6.5 m

Equilibrium

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

ΣMA = 0: RB·5 = 75·3 + 36·6.5
RB = 459/5 = 91.8 kN
RA = 111 − 91.8 = 19.2 kN

Answer

RB = 91.8 kN
3.Truss: method of joints

Answer: FAC = 11.72 kN

Method of joints: every pin of a truss is in equilibrium, so ΣFx = 0 and ΣFy = 0 at each joint. Start at a joint with at most two unknown member forces. A negative result means the member is in compression.

ABBCACACB25 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 25·3 → Cy = 9.375 kN
ΣFy = 0: Ay = 25 − 9.375 = 15.63 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 = 4/6.403 = 0.6247, cos γ = 5/6.403 = 0.7809
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −9.375/0.6247 = −15.01 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−15.01)·0.7809 = 11.72 kN

Answer

FAC = 11.72 kN (tension)
4.Truss: method of joints

Answer: FAB = −17.95 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.

ABBCACACB60 kN10 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 60·5 + 10·2 → Cy = 53.33 kN
ΣFy = 0: Ay = 60 − 53.33 = 6.667 kN
ΣFx = 0: Ax = −10 kN

Joint A

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

sin α = 2/5.385 = 0.3714
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −6.667/0.3714 = −17.95 kN

Answer

FAB = −17.95 kN (compression)
5.Shear force & bending moment

Answer: Vx = −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 = 5·5 = 25 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 5·5·2.5
RB = 62.5/5 = 12.5 kN
ΣFy = 0: RA = 25 − 12.5 = 12.5 kN
w = 5 kN/mABRA​ = 12.5RB​ = 12.5section3.5 m1.5 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 = 12.5 − 5·3.5 = −5 kN

Answer

Vx = −5 kN
6.Shear force & bending moment

Answer: E (x = 4 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 = 7.5 kN, R2 = 67.5 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 = 7.5, MC = 15, MD = 22.5, ME = −30 kN·m, MF = −15, MG = 0

Answer

Mark E: ME = −30 kN·m
7.Beam deflection

Answer: δmax = 26.74 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 = 12 N/mm, L = 2000 mm
EI = 9.35 × 10¹⁰ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·12·2000⁴/(384·9.35 × 10¹⁰) = 26.74 mm

Answer

δmax = 26.74 mm
8.Beam deflection

Answer: Ireq = 167.4 × 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 = 5000/360 = 13.89 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·20·5000⁴/(384·70000·13.89) = 1.674 × 10⁸ mm⁴
Ireq = 167.4 × 10⁶ mm⁴

Answer

Ireq = 167.4 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 38.59 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·40⁴/64 = 125664 mm⁴

Effective length

KL = 1·1500 = 1500 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·125664/1500² = 38586 N = 38.59 kN

Answer

Pcr = 38.59 kN
10.Column buckling

Answer: d = 60.52 mm

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.

Required critical load

Pcr = n·P = 2.5·130000 = 325000 N
KL = 0.5·4000 = 2000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·325000·2000²/(π³·200000))^(1/4) = 60.52 mm

Answer

d = 60.52 mm

Check: the slenderness KL/r is 132.2, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: r = 136.9 mm

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. The radius of gyration r = √(I/A) is the distance at which the whole area would give the same I; it is used in column buckling.

Net area and second moment of area

b = 108 mm, h = 388 mm
A = BH − bh = 120·400 − 108·388 = 6096 mm²
I = (BH³ − bh³)/12 = 1.143 × 10⁸ mm⁴

Radius of gyration

r = √(I/A) = √(1.143 × 10⁸/6096) = 136.9 mm

Answer

r = 136.9 mm
12.Centroid & second moment of area

Answer: σbottom = 194.5 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 = 140·10 = 1400 mm², yf = 140 + 10/2 = 145 mm
web: Aw = 14·140 = 1960 mm², yw = 140/2 = 70 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (1400·145 + 1960·70)/3360 = 101.3 mm

Parallel-axis theorem

flange: 140·10³/12 + 1400·(145 − 101.3)² = 2.691 × 10⁶ mm⁴
web: 14·140³/12 + 1960·(70 − 101.3)² = 5.115 × 10⁶ mm⁴
Ix = 2.691 × 10⁶ + 5.115 × 10⁶ = 7.807 × 10⁶ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 101.3 mm
σ = M·y/I = 1.5 × 10⁷·101.3/7.807 × 10⁶ = 194.5 MPa

Answer

σbottom = 194.5 MPa
13.Effective stress in soil

Answer: σ′ = 91.14 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) = 16.5·2 + 19.5·6 = 150 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·6 = 58.86 kPa

Effective stress

σ′ = σ − u = 150 − 58.86 = 91.14 kPa

Answer

σ′ = 91.14 kPa
14.Effective stress in soil

Answer: σ′ = 64.29 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).

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·2 + γsat,clay·3.5
σ = 16·1 + 20.5·2 + 17.5·3.5 = 118.3 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·5.5 = 53.96 kPa

Effective stress

σ′ = σ − u = 118.3 − 53.96 = 64.29 kPa

Answer

σ′ = 64.29 kPa
15.Consolidation settlement

Answer: S = 195.1 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 = 55 + 50 = 105 kPa > 85 kPa

Settlement

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

S = 0.06·7.5/(1 + 1.2)·log₁₀(85/55) + 0.5·7.5/(1 + 1.2)·log₁₀(105/85)
S = 38.67 + 156.4 = 195.1 mm

Answer

S = 195.1 mm
16.Consolidation settlement

Answer: t = 1.703 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 = 6.5/2 = 3.25 m

Time

t = Tv·Hdr²/cv = 0.403·3.25²/2.5 = 1.703 years

Answer

t = 1.703 years
17.Hydrostatic force

Answer: F = 18.39 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 + 1.5/2 = 1.25 m
A = H·b = 1.5·1 = 1.5 m²
gated = 0.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·1.25·1.5 = 18.39 kN

Answer

F = 18.39 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 = 3·1.5 = 4.5 m²
gated = 2.5 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·4·4.5 = 222.5 kN

Centre of pressure

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

Ic = b·H³/12 = 1.5·3³/12 = 3.375 m⁴
ycp = yc + Ic/(yc·A) = 4 + 3.375/(4·4.5) = 4.188 m

Answer

ycp = 4.188 m
19.Pipe friction & head loss

Answer: hf = 6.529 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·0.075²/4 = 0.004418 m²
V = Q/A = 0.005/0.004418 = 1.132 m/s

Velocity head

V²/(2g) = 1.132²/(2·9.81) = 0.06529 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.025·(300/0.075)·1.132²/(2·9.81) = 6.529 m

Answer

hf = 6.529 m
20.Pipe friction & head loss

Answer: Δz = 3.736 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 = 0.075/0.04909 = 1.528 m/s
V²/(2g) = 0.119 m

Loss coefficients

f·L/D = 0.02·300/0.25 = 24
ΣK = 0.5 + 3·0.3 + 5 + 1.0 = 7.4

Total head loss

hf = 24·0.119 = 2.856 m
hm = 7.4·0.119 = 0.8805 m
Δz = hf + hm = 3.736 m

Answer

Δz = 3.736 m
21.Open-channel flow (Manning)

Answer: Q = 0.5725 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 = 0.3181 m², R = D/4 = 0.225 m

Velocity

V = (1/0.013)·0.2252/3·0.0041/2 = 1.8 m/s

Flow rate

Q = A·V = 0.3181·1.8 = 0.5725 m³/s

Answer

Q = 0.5725 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.004885 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·y = 2·0.5 = 1 m²
P = b + 2y = 2 + 2·0.5 = 3 m
R = A/P = 0.3333 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.014·2.4/(1·0.4807) = 0.06989
S = 0.06989² = 0.004885

Answer

S = 0.004885

That is a fall of 4.885 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 73.25 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 = 1000·9.81·0.08·70 = 54.94 kW

Shaft power

Pshaft = Ph/η = 54.94/0.75 = 73.25 kW

Answer

Pshaft = 73.25 kW
24.Pumps & pump power

Answer: H = 41.41 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (7.2 + 6)·0.3046 = 4.021 m

Pressure head

p/(ρ·g) = 200000/(1000·9.81) = 20.39 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 17 + 20.39 + 4.021 = 41.41 m

Answer

H = 41.41 m
25.Time value of money

Answer: PV = 7413 €

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 = 0.05/12 = 0.004167
N = 12·6 = 72

Present value

PV = FV/(1 + i)N = 10 000/1.349 = €7 412.80

Answer

PV = €7 412.80
26.Time value of money

Answer: B = 235460 €

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 payment

i = 0.0035, N = 300
A = 300 000·0.0035/(1 − (1 + 0.0035)−300) = €1 616.83

Present value of the remaining payments

Whatever is still owed must be exactly paid off by the remaining payments.

N − k = 300 − 96 = 204
B = 1617·(1 − (1 + 0.0035)−204)/0.0035 = €235 459.73

Answer

B = €235 459.73
27.NPV & IRR

Answer: DPB = 3.43 years

Payback period: the time until the cumulative cash flows repay the initial investment. Cash is assumed to come in evenly during each year, so the last part is a fraction of a year. The simple payback ignores the time value of money; the discounted payback period uses the discounted cash flows instead.

Discounted and cumulative cash flows

year 1: 6 500/1.05 = 6 190.48 → Σ = 6 190.48
year 2: 6 500/1.103 = 5 895.69 → Σ = 12 086.17
year 3: 6 500/1.158 = 5 614.94 → Σ = 17 701.11
year 4: 6 500/1.216 = 5 347.57 → Σ = 23 048.68

Fraction of the last year

DPB = 3 + 2 298.89/5 347.57 = 3.43

Answer

DPB = 3.43 years

The discounted payback is always longer than the simple payback (3.077 years).

28.NPV & IRR

Answer: IRR = 38.83 %

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(35%) = 1 067.42
NPV(40%) = −306.12

Narrow down

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

IRR ≈ 35 + 5·1 067.42/(1 067.42 − (−306.12)) = 38.89%
exact: NPV(38.83%) = 0 → IRR = 38.83%

Answer

IRR = 38.83%
29.Normal distribution

Answer: P = 0.06426

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 sum

μ = 32 min, σ = √(1.5² + 2²) = 2.5 min

Standardise

z = (35.8 − 32)/2.5 = 1.52

Upper tail

P = 1 − Φ(1.52) = 1 − 0.9357 = 0.06426

Answer

P = 0.06426
30.Normal distribution

Answer: x = 48.55 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) = 0.05 → z = −1.645

Back to x

x = 65 + −1.645·10 = 48.55 points

Answer

x = 48.55 points

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