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​ = 60 kNP2​ = 30 kNABRA​RB​ = ?1 m0.5 m3.5 m

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

L = 5 mP1 = 60 kN at 1 mP2 = 30 kN at 1.5 m
RB = kN
2.Beam support reactionsHard
w = 2 kN/mP = 25 kNABRA​ = ?RB​1 m3 m

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

L = 4 mP = 25 kN at 1 mw = 2 kN/m from 0 to 4 m
RA = kN
3.Truss: method of jointsMedium
ABCDEFGH35 kN15 kN30 kN4 × 3 m3 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

B: 35 kN ↓C: 15 kN ↓G: 30 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member FC
  13. 13member HC
4.Truss: method of jointsHard
ABBCACACB40 kN20 kN5 m3 m3 m

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

span = 5 mheight = 3 mB is 3 m from Avertical load = 40 kNhorizontal load = 20 kN ←
FBC = kN
5.Shear force & bending momentMedium
w = 3 kN/mABsection2 m8 m

Find the bending moment Mx at the section x = 2 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mw = 3 kN/m from 0 to 10 mx = 2 m
Mx = kN·m
6.Shear force & bending momentHard
w = 6 kN/mP = 25 kNABsection1 m5 m2 m

Find the bending moment Mx at the section x = 1 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 25 kN at 6 mw = 6 kN/m from 0 to 8 mx = 1 m
Mx = kN·m
7.Beam deflectionMedium
P = 3 kNABδ1.5 m1 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 = 3 kNa = 1.5 mL = 2.5 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
w = 2.5 kN/mABδ3 m

A simply supported timber beam of rectangular section, 100 mm wide, carries a uniformly distributed load w over its whole span. Its midspan deflection may not exceed span/360. Find the smallest depth hreq of the section.

w = 2.5 kN/mL = 3 mE = 11 GPa (timber)b = 100 mm
hreq = mm
9.Column bucklingMedium
PL = 2 m40 × 100 mmcross-section

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

L = 2 mE = 70 GPa (aluminium)b × h = 40 × 100 mm
Pcr = kN
10.Column bucklingHard
PL = 3 md = 20 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 = 20 mm
σcr = MPa
11.Centroid & second moment of areaMedium
120 mm300 mm90 mmØ60xIx​ = ?

A 120 mm × 300 mm plate has a circular hole of diameter 60 mm on its vertical centre line, with its centre 90 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 120 mmh = 300 mmd = 60 mmhole centre: y = 90 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
100 mm150 mm45 mm50 × 20xIx​ = ?

A 100 mm × 150 mm plate has a rectangular cut-out 50 mm wide and 20 mm high, centred on the vertical centre line with its centre 45 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 100 mmh = 150 mmcut-out: 50 × 20 mmhole centre: y = 45 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 20.5 kN/m³13 mwater tableXz = 8 m

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

z = 8 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20.5 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 18.5 kN/m³6 mclayγsat​ = 17 kN/m³5 mwater tableXz = 8.5 m

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

z = 8.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 18.5 kN/m³clay: γsat = 17 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 220 kPasandclayCc​ = 0.25, Cr​ = 0.02e0​ = 0.8σ′0​ = 65 kPaσ′p​ = 155 kPa4 mwater table

A 4 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.02 and e₀ = 0.8. At its mid-depth the effective vertical stress is 65 kPa and the preconsolidation pressure is 155 kPa. A new building adds 220 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 4 mCc = 0.25Cr = 0.02e0 = 0.8σ′0 = 65 kPaσ′p = 155 kPaΔσ = 220 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 3.5 m3.5 msandwater table

In a laboratory oedometer test, a clay specimen 20 mm thick, drained at the top and bottom, reaches 50% consolidation in 10 min. In the field the same clay forms a layer 3.5 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 = 20 mmtlab = 10 minH = 3.5 mfield: double drainage
t = days
17.Hydrostatic forceMedium
gated = 1 mH = 3 m

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

d = 1 mH = 3 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 4 mH = 2.5 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of glycerin, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 2.5 mb = 3 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1.4 m/sD = 200 mmL = 200 mf = 0.025

Water (ρ = 1000 kg/m³) flows at 1.4 m/s through a horizontal pipe, 200 m long, with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.025 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1.4 m/sL = 200 mD = 200 mmf = 0.025ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 5Δz = ?L = 150 m, D = 150 mm, f = 0.0223× bend (K = 0.3)

Two open reservoirs are joined by a pipe 150 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.022. 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 60 L/s?

Q = 60 L/sL = 150 mD = 150 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 2.5 my = 2 m1.5 : 1n = 0.015, S = 0.001

A trapezoidal brickwork channel has a bottom width of 2.5 m and side slopes of 1.5:1 (horizontal:vertical). Water flows uniformly 2 m deep. Manning n = 0.015 and the bed slope is S = 0.001. Find the flow rate Q in m³/s.

b = 2.5 my = 2 mz = 1.5n = 0.015S = 0.001
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 4 my = 1.2 mn = 0.012, Q = 15 m³/s

A rectangular finished concrete channel 4 m wide must carry 15 m³/s in uniform flow at a depth of 1.2 m. Manning n = 0.012. Find the required bed slope S (in m/m).

Q = 15 m³/sb = 4 my = 1.2 mn = 0.012
S = m/m
23.Pumps & pump powerMedium
PQ = 15 L/sH = 80 m

A pump with an efficiency of 72% delivers 15 L/s of water (ρ = 1000 kg/m³) against a head of 80 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 15 L/sH = 80 mη = 72%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 50 L/sΔz = 16 mL = 500 m, D = 150 mm, f = 0.02, ΣK = 6

A pump moves 50 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 16 m higher. The pipe is 500 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 65%. Find the shaft power Pshaft in kW.

Q = 50 L/sΔz = 16 mL = 500 mD = 150 mmf = 0.02ΣK = 6η = 65%
Pshaft = kW
25.Time value of moneyMedium
years0123…9PV = ?€10 000+1%+1%…r = 3%

A property is expected to earn net rent of €10 000 next year. The rent is expected to grow by 1% per year forever. The required return is 3% per year. Find the value PV of the property today.

C1 = €10 000g = 1%r = 3%
PV = €
26.Time value of moneyHard
months0123…36€20 000A?AAA

A loan of €20 000 is repaid with equal monthly payments over 3 years. The interest rate is 5.4% per year, compounded monthly. Find the monthly payment A.

P = €20 0005.4% / 12N = 36
A = €
27.NPV & IRRMedium
years012345−20 0005 0005 0005 0005 0005 000

A project costs €20 000 today and returns €5 000 at the end of each year for 5 years. 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 = −20 000CF1 = 5 000CF2 = 5 000CF3 = 5 000CF4 = 5 000CF5 = 5 000
DPB = years
28.NPV & IRRHard
years0123−40 00030 00017 00027 500

A project costs €40 000 and returns €30 000, €17 000, €27 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 30 000CF2 = 17 000CF3 = 27 500
IRR = %
29.Normal distributionMedium
480550P = ?

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. What fraction lies between 480 and 550 h? Give P as a decimal.

μ = 500σ = 40x1 = 480x2 = 550
P =
30.Normal distributionHard
557085100115130145pointstop 60%

The IQ scores are normally distributed with mean 100 points and standard deviation 15 points. Drag the cut-off so the shaded top 60% is to the right of it. Find the cut-off x.

μ = 100 pointsσ = 15 points60%
x = points

3Solutions

1.Beam support reactions

Answer: RB = 21 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​ = 60 kNP2​ = 30 kNABRA​RB​1 m0.5 m3.5 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·5 = 60·1 + 30·1.5
RB = 105/5 = 21 kN
ΣFy = 0: RA = 90 − 21 = 69 kN

Answer

RB = 21 kN
2.Beam support reactions

Answer: RA = 22.75 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.

w = 2 kN/mP = 25 kNABRA​RB​1 m3 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 = 2·4 = 8 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 25·1 + 2·4·2
RB = 41/4 = 10.25 kN
ΣFy = 0: RA = 33 − 10.25 = 22.75 kN

Answer

RA = 22.75 kN
3.Truss: method of joints

Answer: member DH

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint D

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

ΣF⊥ = 0 → FDH = 0

Check with the method of joints

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

AB: 48.75 kN (T), BC: 48.75 kN (T), CD: 31.25 kN (T), DE: 31.25 kN (T), FG: 62.5 kN (C), GH: 62.5 kN (C), AF: 68.94 kN (C), HE: 44.19 kN (C), BF: 35 kN (T), CG: 30 kN (C), DH: 0, FC: 19.45 kN (T), HC: 44.19 kN (T)

Answer

Zero-force member: DH
4.Truss: method of joints

Answer: FBC = −14.42 kN

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

ABBCACACB40 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 40·3 − 20·3 → Cy = 12 kN
ΣFy = 0: Ay = 40 − 12 = 28 kN
ΣFx = 0: Ax = 20 kN

Joint C

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

sin γ = 3/3.606 = 0.8321, cos γ = 2/3.606 = 0.5547
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −12/0.8321 = −14.42 kN

Answer

FBC = −14.42 kN (compression)
5.Shear force & bending moment

Answer: Mx = 24 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 = 3·10 = 30 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 3·10·5
RB = 150/10 = 15 kN
ΣFy = 0: RA = 30 − 15 = 15 kN
w = 3 kN/mABRA​ = 15RB​ = 15section2 m8 m

Cut at x = 2 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 = 15·2 − 3·2·1 = 24 kN·m

Answer

Mx = 24 kN·m
6.Shear force & bending moment

Answer: Mx = 27.25 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 = 6·8 = 48 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 25·6 + 6·8·4
RB = 342/8 = 42.75 kN
ΣFy = 0: RA = 73 − 42.75 = 30.25 kN
w = 6 kN/mP = 25 kNABRA​ = 30.25RB​ = 42.75section1 m5 m2 m

Cut at x = 1 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 = 30.25·1 − 6·1·0.5 = 27.25 kN·m

Answer

Mx = 27.25 kN·m
7.Beam deflection

Answer: δB = 2.813 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 = 3000 N, a = 1500 mm, L = 2500 mm
EI = 2.4 × 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) = 1.406 mm
θP = Pa²/(2EI) = 0.001406 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 2.813 mm

Answer

δB = 2.813 mm
8.Beam deflection

Answer: hreq = 151.1 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 = 2.5 N/mm, L = 3000 mm, E = 11000 N/mm²

Deflection limit

δallow = L/360 = 3000/360 = 8.333 mm

Required second moment of area

Ireq = 5wL⁴/(384·E·δallow) = 5·2.5·3000⁴/(384·11000·8.333) = 2.876 × 10⁷ mm⁴

Required depth

bh³/12 = Ireq → h = (12·2.876 × 10⁷/100)1/3 = 151.1 mm

Answer

hreq = 151.1 mm

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

9.Column buckling

Answer: Pcr = 23.03 kN

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

Smallest second moment of area

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

Imin = h·b³/12 = 100·40³/12 = 533333 mm⁴

Effective length

KL = 2·2000 = 4000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·533333/4000² = 23029 N = 23.03 kN

Answer

Pcr = 23.03 kN
10.Column buckling

Answer: σcr = 11.19 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·20⁴/64 = 7854 mm⁴

Radius of gyration and slenderness

A = 314.2 mm²
r = √(I/A) = √(7854/314.2) = 5 mm
KL = 0.7·3000 = 2100 mm
KL/r = 2100/5 = 420

Critical stress

σcr = π²E/(KL/r)² = π²·200000/420² = 11.19 MPa

Answer

σcr = 11.19 MPa
11.Centroid & second moment of area

Answer: Ix = 258.3 × 10⁶ mm⁴

Sections with holes: treat a hole as a negative area. The centroid is ȳ = (A₁y₁ − A₂y₂)/(A₁ − A₂), with A₁, y₁ for the full plate and A₂, y₂ for the hole. For the second moment of area about the centroidal axis, use the parallel-axis theorem for each part and subtract the hole: I = (Ic1 + A₁d₁²) − (Ic2 + A₂d₂²), where d is the distance from each part's own centroid to the axis through ȳ. A rectangle has Ic = bh³/12 and a circle Ic = πd⁴/64.

Centroid

ȳ = (36000·150 − 2827·90)/(36000 − 2827) = 155.1 mm

Full plate about ȳ

120·300³/12 + 36000·−5.114² = 270.9 × 10⁶ mm⁴

Hole about ȳ

π·60⁴/64 + 2827·−65.11² = 12.62 × 10⁶ mm⁴

Subtract

Ix = 258.3 × 10⁶ mm⁴

Answer

Ix = 258.3 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 27.13 × 10⁶ mm⁴

Sections with holes: treat a hole as a negative area. The centroid is ȳ = (A₁y₁ − A₂y₂)/(A₁ − A₂), with A₁, y₁ for the full plate and A₂, y₂ for the hole. For the second moment of area about the centroidal axis, use the parallel-axis theorem for each part and subtract the hole: I = (Ic1 + A₁d₁²) − (Ic2 + A₂d₂²), where d is the distance from each part's own centroid to the axis through ȳ. A rectangle has Ic = bh³/12 and a circle Ic = πd⁴/64.

Centroid

ȳ = (15000·75 − 1000·45)/(15000 − 1000) = 77.14 mm

Full plate about ȳ

100·150³/12 + 15000·−2.143² = 28.19 × 10⁶ mm⁴

Hole about ȳ

50·20³/12 + 1000·−32.14² = 1.066 × 10⁶ mm⁴

Subtract

Ix = 27.13 × 10⁶ mm⁴

Answer

Ix = 27.13 × 10⁶ mm⁴
13.Effective stress in soil

Answer: u = 58.86 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) = 9.81·6 = 58.86 kPa

Answer

u = 58.86 kPa
14.Effective stress in soil

Answer: σ′ = 84.73 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·4 + γsat,clay·2.5
σ = 16·2 + 18.5·4 + 17·2.5 = 148.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·6.5 = 63.77 kPa

Effective stress

σ′ = σ − u = 148.5 − 63.77 = 84.73 kPa

Answer

σ′ = 84.73 kPa
15.Consolidation settlement

Answer: S = 163.7 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 = 65 + 220 = 285 kPa > 155 kPa

Settlement

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

S = 0.02·4/(1 + 0.8)·log₁₀(155/65) + 0.25·4/(1 + 0.8)·log₁₀(285/155)
S = 16.77 + 147 = 163.7 mm

Answer

S = 163.7 mm
16.Consolidation settlement

Answer: t = 212.7 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 = 20/2 = 10 mm = 0.01 m
Hdr,field = 3.5/2 = 1.75 m

Scale the time

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

tfield = 10·(1.75/0.01)² = 306250 min
tfield = 306250/1440 = 212.7 days

Answer

t = 212.7 days
17.Hydrostatic force

Answer: F = 73.58 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 = 1 + 3/2 = 2.5 m
A = H·b = 3·1 = 3 m²
gated = 1 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.5·3 = 73.58 kN

Answer

F = 73.58 kN
18.Hydrostatic force

Answer: F = 486.7 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 = 4 + 2.5/2 = 5.25 m
A = H·b = 2.5·3 = 7.5 m²
gated = 4 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·5.25·7.5 = 486.7 kN

Answer

F = 486.7 kN
19.Pipe friction & head loss

Answer: Δp = 24.5 kPa

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

Head loss

hf = f·(L/D)·V²/(2g) = 0.025·(200/0.2)·1.4²/(2·9.81) = 2.497 m

Pressure drop

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

Δp = ρ·g·hf = 1000·9.81·2.497 = 24500 Pa = 24.5 kPa

Answer

Δp = 24.5 kPa
20.Pipe friction & head loss

Answer: Δz = 17.27 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 = 0.06/0.01767 = 3.395 m/s
V²/(2g) = 0.5876 m

Loss coefficients

f·L/D = 0.022·150/0.15 = 22
ΣK = 0.5 + 3·0.3 + 5 + 1.0 = 7.4

Total head loss

hf = 22·0.5876 = 12.93 m
hm = 7.4·0.5876 = 4.348 m
Δz = hf + hm = 17.27 m

Answer

Δz = 17.27 m
21.Open-channel flow (Manning)

Answer: Q = 25.2 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 = (2.5 + 1.5·2)·2 = 11 m²
P = b + 2y·√(1 + z²) = 2.5 + 2·2·√(1 + 1.5²) = 9.711 m
R = A/P = 1.133 m

Velocity

V = (1/0.015)·1.1332/3·0.0011/2 = 2.291 m/s

Flow rate

Q = A·V = 11·2.291 = 25.2 m³/s

Answer

Q = 25.2 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002064 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 = 4·1.2 = 4.8 m²
P = b + 2y = 4 + 2·1.2 = 6.4 m
R = A/P = 0.75 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.012·15/(4.8·0.8255) = 0.04543
S = 0.04543² = 0.002064

Answer

S = 0.002064

That is a fall of 2.064 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 16.35 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 = 1000·9.81·0.015·80 = 11.77 kW

Shaft power

Pshaft = Ph/η = 11.77/0.72 = 16.35 kW

Answer

Pshaft = 16.35 kW
24.Pumps & pump power

Answer: Pshaft = 34.45 kW

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

Velocity

V = Q/A = 0.05/0.01767 = 2.829 m/s
V²/(2g) = 0.408 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (66.67 + 6)·0.408 = 29.65 m

Pump head

H = Δz + hL = 16 + 29.65 = 45.65 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.05·45.65/0.65 = 34.45 kW

Answer

Pshaft = 34.45 kW
25.Time value of money

Answer: PV = 500000 €

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.

Growing perpetuity

PV = C1/(r − g) = 10 000/(0.03 − 0.01) = 10 000/0.02 = €500 000.00

Answer

PV = €500 000.00
26.Time value of money

Answer: A = 603 €

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 payments

i = 0.054000000000000006/12 = 0.0045
N = 12·3 = 36

Payment

The present value of N equal payments A is A·(1 − (1 + i)⁻ᴺ)/i. Set it equal to the loan and solve for A.

(1 + i)−N = 0.8508
A = 20 000·0.0045/(1 − 0.8508) = €603.02

Answer

A = €603.02
27.NPV & IRR

Answer: DPB = 4.716 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: 5 000/1.06 = 4 716.98 → Σ = 4 716.98
year 2: 5 000/1.124 = 4 449.98 → Σ = 9 166.96
year 3: 5 000/1.191 = 4 198.10 → Σ = 13 365.06
year 4: 5 000/1.262 = 3 960.47 → Σ = 17 325.53
year 5: 5 000/1.338 = 3 736.29 → Σ = 21 061.82

Fraction of the last year

DPB = 4 + 2 674.47/3 736.29 = 4.716

Answer

DPB = 4.716 years

The discounted payback is always longer than the simple payback (4 years).

28.NPV & IRR

Answer: IRR = 40.25 %

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(40%) = 123.91
NPV(45%) = −2 204.27

Narrow down

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

IRR ≈ 40 + 5·123.91/(123.91 − (−2 204.27)) = 40.27%
exact: NPV(40.25%) = 0 → IRR = 40.25%

Answer

IRR = 40.25%
29.Normal distribution

Answer: P = 0.5858

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 = (480 − 500)/40 = −0.5
z₂ = (550 − 500)/40 = 1.25

Area between

P = Φ(1.25) − Φ(−0.5) = 0.8944 − 0.3085 = 0.5858

Answer

P = 0.5858
30.Normal distribution

Answer: x = 96.3 points

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) = 0.4

z from the table

z ≈ −0.25

Back to the original units

x = 100 − 0.25·15 = 96.3 points

Answer

x = 96.3 points

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