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​ = 35 kNP2​ = 35 kNABRA​RB​ = ?3 m4 m1 m

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

L = 8 mP1 = 35 kN at 3 mP2 = 35 kN at 7 m
RB = kN
2.Beam support reactionsHard
w = 4 kN/mP = 60 kNABRA​ = ?RB​2 m1.5 m0.5 m1 m

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

L = 5 mP = 60 kN at 3.5 mw = 4 kN/m from 2 to 4 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB35 kN4 m3 m2 m

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

span = 4 mheight = 2 mB is 3 m from Avertical load = 35 kN
FAC = kN
4.Truss: method of jointsHard
ABBCACACB35 kN5 kN8 m3 m4 m

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

span = 8 mheight = 4 mB is 3 m from Avertical load = 35 kNhorizontal load = 5 kN ←
FAB = kN
5.Shear force & bending momentMedium
P1​ = 60 kNP2​ = 80 kNAB4 m2 m2 m

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

L = 8 mP1 = 60 kN at 4 mP2 = 80 kN at 6 m
Mmax = kN·m
6.Shear force & bending momentHard
w = 6 kN/mABC8 m2.5 m

The beam rests on a pin at A and a roller at B and overhangs B by 2.5 m to the free end C. A uniformly distributed load w acts over the whole length A–C. Find the maximum sagging bending moment Mmax between the supports.

L = 10.5 mw = 6 kN/m from 0 to 10.5 msupports at x = 0 and x = 8 m
Mmax = kN·m
7.Beam deflectionMedium
w = 2 kN/mδL = 3 m

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

w = 2 kN/mL = 3 mE = 70 GPa (aluminium)I = 84 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 10 kN/mδL = 2.5 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 = 10 kN/mL = 2.5 mE = 70 GPa (aluminium)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 4 m30 × 80 mmcross-section

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

L = 4 mE = 70 GPa (aluminium)b × h = 30 × 80 mm
Pcr = kN
10.Column bucklingHard
P = 140 kNL = 4 md = ?cross-section

A solid round column of length L made of steel is fixed at both ends. It must carry 140 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 140 kNn = 2L = 4 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
2401524020xdimensions in mm

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

bf = 240 mmtf = 15 mmtw = 20 mmhw = 240 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
150280163202212xdimensions in mm

A welded I-section has a top flange 150 × 16 mm, a web 320 mm high and 12 mm thick, and a bottom flange 280 × 22 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 150 × 16 mmweb: 12 × 320 mmbottom flange: 280 × 22 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 20 kN/m³6 mwater tableXz = 6 m

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

z = 6 mzw = 4 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 20 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 19 kN/m³4 mclayγsat​ = 17 kN/m³5 mwater tableXz = 6.5 m

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

z = 6.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19 kN/m³clay: γsat = 17 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 50 kPasandclayCc​ = 0.5, Cr​ = 0.04e0​ = 1.1σ′0​ = 100 kPaσ′p​ = 190 kPa2 mwater table

A 2 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.04 and e₀ = 1.1. At its mid-depth the effective vertical stress is 100 kPa and the preconsolidation pressure is 190 kPa. A new building adds 50 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2 mCc = 0.5Cr = 0.04e0 = 1.1σ′0 = 100 kPaσ′p = 190 kPaΔσ = 50 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 8.5 mcv​ = 2 m²/year8.5 mimpervious rockwater table

A clay layer 8.5 m thick has a coefficient of consolidation cv = 2 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 90% average consolidation the time factor is Tv = 0.848. How many years t does the layer take to reach 90% consolidation?

H = 8.5 mcv = 2 m²/yearU = 90%Tv = 0.848single drainage
t = years
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 = 2 m

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

d = 3 mH = 2 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
Q = 40 L/sD = 200 mmL = 800 mf = 0.018

Water flows at 40 L/s through a pipe 800 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.018 and g = 9.81 m/s². Find the friction head loss hf.

Q = 40 L/sL = 800 mD = 200 mmf = 0.018g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2Δz = 16 mL = 200 m, D = 250 mm, f = 0.0154× bend (K = 0.3)

Two open reservoirs are joined by a pipe 200 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.015. The water surface of the upper reservoir is 16 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 = 2) 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 = 16 mL = 200 mD = 250 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 2Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 4.5 my = 1.8 m3 : 1n = 0.022, S = 0.005

A trapezoidal clean earth channel has a bottom width of 4.5 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 1.8 m deep. Manning n = 0.022 and the bed slope is S = 0.005. Find the flow rate Q in m³/s.

b = 4.5 my = 1.8 mz = 3n = 0.022S = 0.005
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 5 my = 1.3 mn = 0.012, Q = 14 m³/s

A rectangular finished concrete channel 5 m wide must carry 14 m³/s in uniform flow at a depth of 1.3 m. Manning n = 0.012. Find the required bed slope S (in m/m).

Q = 14 m³/sb = 5 my = 1.3 mn = 0.012
S = m/m
23.Pumps & pump powerMedium
PQ = 40 L/sH = 80 m

In a test, a pump delivers 40 L/s of water (ρ = 1000 kg/m³) against a head of 80 m while its shaft takes 40.2 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 40 L/sH = 80 mPshaft = 40.2 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
300 kPa (gauge)PQ = 40 L/sΔz = 27 mL = 100 m, D = 150 mm, f = 0.018, ΣK = 8

A pump moves 40 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 27 m higher. The pipe is 100 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 300 kPa. Find the head H the pump must add.

Q = 40 L/sΔz = 27 mL = 100 mD = 150 mmf = 0.018ΣK = 8ptank = 300 kPa
H = m
25.Time value of moneyMedium
years0123456PV = ?€5 000

You need €5 000 in 6 years. An account pays 3% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €5 0003% / 4n = 6
PV = €
26.Time value of moneyHard
months0123…204€250€250€250FV = ?

You save €250 at the end of every month for 17 years. The account pays 2.4% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €2502.4% / 12N = 204
FV = €
27.NPV & IRRMedium
years012345−50 00020 00020 00017 50014 00019 000

A project costs €50 000 today and returns €20 000, €20 000, €17 500, €14 000, €19 000 at the end of years 1 to 5. The cost of capital is 6%. Assume cash flows arrive evenly through each year. Find the discounted payback period DPB in years.

r = 6%CF0 = −50 000CF1 = 20 000CF2 = 20 000CF3 = 17 500CF4 = 14 000CF5 = 19 000
DPB = years
28.NPV & IRRHard
years0123…10−200 00022 000+4%+4%+4%r = 8%, NPV = ?

A project costs €200 000 today. Its cash flow is €22 000 at the end of year 1 and grows by 4% per year until the last cash flow at the end of year 10. The cost of capital is 8%. Find the net present value NPV.

C0 = €200 000CF1 = €22 000g = 4%n = 10r = 8%
NPV = €
29.Normal distributionMedium
−3−2−10123zshaded area to the right of z = 0.9850

Drag z so that the shaded area under the standard normal curve, to the right of z, is 0.9850. Find z to two decimals.

A = 0.9850
z =
30.Normal distributionHard
157164171178185192199cmbottom 60%

The heights of adult men are normally distributed with mean 178 cm and standard deviation 7 cm. Drag the cut-off so the shaded bottom 60% is to the left of it. Find the cut-off x.

μ = 178 cmσ = 7 cm60%
x = cm

3Solutions

1.Beam support reactions

Answer: RB = 43.75 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​ = 35 kNP2​ = 35 kNABRA​RB​3 m4 m1 m

Free-body diagram

Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.

Equilibrium

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

ΣMA = 0: RB·8 = 35·3 + 35·7
RB = 350/8 = 43.75 kN
ΣFy = 0: RA = 70 − 43.75 = 26.25 kN

Answer

RB = 43.75 kN
2.Beam support reactions

Answer: RA = 21.2 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Taking moments about one support removes that support’s reaction from the equation.

w = 4 kN/mP = 60 kNABRA​RB​2 m1.5 m0.5 m1 m

Free-body diagram

Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.

Equilibrium

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

UDL resultant: W = w·ℓ = 4·2 = 8 kN, acting at x̄ = 3 m
ΣMA = 0: RB·5 = 60·3.5 + 4·2·3
RB = 234/5 = 46.8 kN
ΣFy = 0: RA = 68 − 46.8 = 21.2 kN

Answer

RA = 21.2 kN
3.Truss: method of joints

Answer: FAC = 13.13 kN

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

ABBCACACB35 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·4 = 35·3 → Cy = 26.25 kN
ΣFy = 0: Ay = 35 − 26.25 = 8.75 kN

Joint C

The roller gives only a vertical reaction, so joint C has just two unknown member forces. Assume both in tension.

sin γ = 2/2.236 = 0.8944, cos γ = 1/2.236 = 0.4472
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −26.25/0.8944 = −29.35 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−29.35)·0.4472 = 13.13 kN

Answer

FAC = 13.13 kN (tension)
4.Truss: method of joints

Answer: FAB = −30.47 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·8 = 35·3 − 5·4 → Cy = 10.63 kN
ΣFy = 0: Ay = 35 − 10.63 = 24.38 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 = 4/5 = 0.8
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −24.38/0.8 = −30.47 kN

Answer

FAB = −30.47 kN (compression)
5.Shear force & bending moment

Answer: Mmax = 200 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 = 60·4 + 80·6
RB = 720/8 = 90 kN
ΣFy = 0: RA = 140 − 90 = 50 kN

Moment under each load

Keep the part left of each load.

under P1: M = RA·4 = 50·4 = 200 kN·m
under P2: M = RB·2 = 90·2 = 180 kN·m

Largest value

Mmax = 200 kN·m (under P1)

Answer

Mmax = 200 kN·m
6.Shear force & bending moment

Answer: Mmax = 39.08 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, including the load on the overhang.

UDL resultant: W = w·ℓ = 6·10.5 = 63 kN, acting at x̄ = 5.25 m
ΣMA = 0: RB·8 = 6·10.5·5.25
RB = 330.8/8 = 41.34 kN
ΣFy = 0: RA = 63 − 41.34 = 21.66 kN

Zero shear

RA − w·x0 = 0 → x0 = 21.66/6 = 3.609 m

Maximum sagging moment

Mmax = RA·x0 − w·x0²/2 = RA²/(2w) = 21.66²/(2·6) = 39.08 kN·m

Answer

Mmax = 39.08 kN·m
7.Beam deflection

Answer: δ = 3.444 mm

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

Consistent units

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

w = 2 N/mm, L = 3000 mm
EI = 5.88 × 10¹² N·mm²

Deflection

δ = wL⁴/(8EI) = 2·3000⁴/(8·5.88 × 10¹²) = 3.444 mm

Answer

δ = 3.444 mm
8.Beam deflection

Answer: Ireq = 10.46 × 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 = 2500/360 = 6.944 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·10·2500⁴/(384·70000·6.944) = 1.046 × 10⁷ mm⁴
Ireq = 10.46 × 10⁶ mm⁴

Answer

Ireq = 10.46 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 15.86 kN

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

Smallest second moment of area

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

Imin = h·b³/12 = 80·30³/12 = 180000 mm⁴

Effective length

KL = 0.7·4000 = 2800 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·180000/2800² = 15862 N = 15.86 kN

Answer

Pcr = 15.86 kN
10.Column buckling

Answer: d = 58.31 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 = 2·140000 = 280000 N
KL = 0.5·4000 = 2000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·280000·2000²/(π³·200000))^(1/4) = 58.31 mm

Answer

d = 58.31 mm

Check: the slenderness KL/r is 137.2, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 56.55 × 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 = 240·15 = 3600 mm², yf = 240 + 15/2 = 247.5 mm
web: Aw = 20·240 = 4800 mm², yw = 240/2 = 120 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3600·247.5 + 4800·120)/8400 = 174.6 mm

Parallel-axis theorem

flange: 240·15³/12 + 3600·(247.5 − 174.6)² = 1.918 × 10⁷ mm⁴
web: 20·240³/12 + 4800·(120 − 174.6)² = 3.737 × 10⁷ mm⁴
Ix = 1.918 × 10⁷ + 3.737 × 10⁷ = 5.655 × 10⁷ mm⁴ = 56.55 × 10⁶ mm⁴

Answer

Ix = 56.55 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 246.8 × 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 three rectangles

Measure every y from the bottom edge.

top flange: A = 2400 mm², y = 350 mm
web: A = 3840 mm², y = 182 mm
bottom flange: A = 6160 mm², y = 11 mm

Centroid

ȳ = (2400·350 + 3840·182 + 6160·11)/12400 = 129.6 mm

Parallel-axis theorem

top flange: 150·16³/12 + 2400·220.4² = 1.167 × 10⁸ mm⁴
web: 12·320³/12 + 3840·52.43² = 4.332 × 10⁷ mm⁴
bottom flange: 280·22³/12 + 6160·118.6² = 8.685 × 10⁷ mm⁴
Ix = 1.167 × 10⁸ + 4.332 × 10⁷ + 8.685 × 10⁷
Ix = 2.468 × 10⁸ mm⁴ = 246.8 × 10⁶ mm⁴

Answer

Ix = 246.8 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ′ = 86.38 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) = 16.5·4 + 20·2 = 106 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·2 = 19.62 kPa

Effective stress

σ′ = σ − u = 106 − 19.62 = 86.38 kPa

Answer

σ′ = 86.38 kPa
14.Effective stress in soil

Answer: σ = 112.5 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·2 + γsat,clay·2.5
σ = 16·2 + 19·2 + 17·2.5 = 112.5 kPa

Answer

σ = 112.5 kPa
15.Consolidation settlement

Answer: S = 6.708 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 = 100 + 50 = 150 kPa ≤ 190 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.04·2/(1 + 1.1)·log₁₀(150/100) = 6.708 mm

Answer

S = 6.708 mm
16.Consolidation settlement

Answer: t = 30.63 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 = 8.5 m

Time

t = Tv·Hdr²/cv = 0.848·8.5²/2 = 30.63 years

Answer

t = 30.63 years
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 = 4.083 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 + 2/2 = 4 m
A = H·b = 2·3 = 6 m²
gated = 3 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·4·6 = 235.4 kN

Centre of pressure

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

Ic = b·H³/12 = 3·2³/12 = 2 m⁴
ycp = yc + Ic/(yc·A) = 4 + 2/(4·6) = 4.083 m

Answer

ycp = 4.083 m
19.Pipe friction & head loss

Answer: hf = 5.949 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·0.2²/4 = 0.03142 m²
V = Q/A = 0.04/0.03142 = 1.273 m/s

Velocity head

V²/(2g) = 1.273²/(2·9.81) = 0.08263 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.018·(800/0.2)·1.273²/(2·9.81) = 5.949 m

Answer

hf = 5.949 m
20.Pipe friction & head loss

Answer: Q = 212.8 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 = 0.015·200/0.25 = 12
ΣK = 0.5 + 4·0.3 + 2 + 1.0 = 4.7

Energy equation

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

16 = (12 + 4.7)·V²/(2·9.81)
V = √(2·9.81·16/16.7) = 4.336 m/s

Flow rate

Q = V·π·D²/4 = 4.336·0.04909 = 0.2128 m³/s = 212.8 L/s

Answer

Q = 212.8 L/s
21.Open-channel flow (Manning)

Answer: Q = 61.84 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 = (4.5 + 3·1.8)·1.8 = 17.82 m²
P = b + 2y·√(1 + z²) = 4.5 + 2·1.8·√(1 + 3²) = 15.88 m
R = A/P = 1.122 m

Velocity

V = (1/0.022)·1.1222/3·0.0051/2 = 3.47 m/s

Flow rate

Q = A·V = 17.82·3.47 = 61.84 m³/s

Answer

Q = 61.84 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0008229 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 = 5·1.3 = 6.5 m²
P = b + 2y = 5 + 2·1.3 = 7.6 m
R = A/P = 0.8553 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.012·14/(6.5·0.901) = 0.02869
S = 0.02869² = 0.0008229

Answer

S = 0.0008229

That is a fall of 0.8229 m per kilometre.

23.Pumps & pump power

Answer: η = 78.09 %

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

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.04·80 = 31.39 kW

Efficiency

η = Ph/Pshaft = 31.39/40.2 = 78.09%

Answer

η = 78.09%
24.Pumps & pump power

Answer: H = 62.8 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 = 0.04/0.01767 = 2.264 m/s
V²/(2g) = 0.2611 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (12 + 8)·0.2611 = 5.223 m

Pressure head

p/(ρ·g) = 300000/(1000·9.81) = 30.58 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 27 + 30.58 + 5.223 = 62.8 m

Answer

H = 62.8 m
25.Time value of money

Answer: PV = 4179 €

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 = 0.03/4 = 0.0075
N = 4·6 = 24

Present value

PV = FV/(1 + i)N = 5 000/1.196 = €4 179.16

Answer

PV = €4 179.16
26.Time value of money

Answer: FV = 62899 €

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

Monthly rate and number of deposits

i = 0.024/12 = 0.002
N = 12·17 = 204

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 250·(1.503 − 1)/0.002 = €62 899.32

Answer

FV = €62 899.32

You paid in €51 000 yourself; the rest is interest.

27.NPV & IRR

Answer: DPB = 2.907 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: 20 000/1.06 = 18 867.92 → Σ = 18 867.92
year 2: 20 000/1.124 = 17 799.93 → Σ = 36 667.85
year 3: 17 500/1.191 = 14 693.34 → Σ = 51 361.19

Fraction of the last year

DPB = 2 + 13 332.15/14 693.34 = 2.907

Answer

DPB = 2.907 years

The discounted payback is always longer than the simple payback (2.571 years).

28.NPV & IRR

Answer: NPV = −27102 €

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

Present value of the growing annuity

((1.04)/(1.08))10 = 0.6856
PV = 22 000/(0.08 − 0.04)·(1 − 0.6856) = 172 898.27

NPV

NPV = 172 898.27 − 200 000 = −€27 101.73

Answer

NPV = −€27 101.73

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

29.Normal distribution

Answer: z = −2.17

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

Area to the left of z

Φ(z) = 1 − 0.9850 = 0.0150

Read the z-table backwards

Find 0.0150 inside the table and read off z.

z = −2.17

Answer

z = −2.17
30.Normal distribution

Answer: x = 179.8 cm

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

Area to the left

Φ(z) = 0.6

z from the table

z ≈ 0.25

Back to the original units

x = 178 + 0.25·7 = 179.8 cm

Answer

x = 179.8 cm

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