FE Civil exam practice: cram pack

Formula sheets, the key method steps for every topic and 30 practice problems, with full solutions at the back.

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1Formulas and methods

Beam support reactions

Equilibrium
ΣFx = 0, ΣFy = 0, ΣM = 0
Uniform load
resultant w·L at the middle of the load
Moment
M = F·d

Method

  1. Draw a free-body diagram and replace each support by its reactions.
  2. Replace every distributed load by a single force at its centroid.
  3. Take moments about one support to find the reaction at the other.
  4. Use ΣFy = 0 to find the remaining reaction, and check with a second moment equation.

Truss: method of joints

Method of joints
ΣFx = 0, ΣFy = 0 at each joint
Method of sections
ΣM = 0 about a cut point
Member force
positive = tension, negative = compression

Method

  1. Find the support reactions for the whole truss.
  2. Method of joints: start at a joint with at most two unknown member forces and use ΣFx = 0 and ΣFy = 0.
  3. Method of sections: cut through the member you need and take moments about a point where the other unknown members meet.
  4. Assume tension; a negative answer means compression.

Shear force & bending moment

Shear and moment
V = ΣF on one side, M = ΣF·d on one side
Bending stress
σ = M·y/I
Rectangle
I = bh³/12
Section modulus
W = I/ymax
Simply supported, uniform load
Mmax = wL²/8

Method

  1. Find the support reactions from equilibrium of the whole beam.
  2. Cut the beam at the section you need and keep one side.
  3. Shear force: sum of the vertical forces on that side. Bending moment: sum of their moments about the cut.
  4. For the maximum moment, find where the shear force is zero.

Beam deflection

Point load at midspan
δ = PL³/(48EI)
Uniform load, simply supported
δ = 5wL⁴/(384EI)
Cantilever, end load
δ = PL³/(3EI)
Cantilever, uniform load
δ = wL⁴/(8EI)
Superposition
δ = δ1 + δ2

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

Centroid & second moment of area

Centroid
ȳ = ΣAiyi/ΣAi
Rectangle
I = bh³/12
Parallel-axis theorem
I = Ic + A·d²
Composite section
I = Σ(Ic,i + Aidi²)

Effective stress in soil

Total stress
σ = Σγi·hi
Pore water pressure
u = γw·(z − zw)
Effective stress
σ′ = σ − u
Water
γw = 9.81 kN/m³

Consolidation settlement

Normally consolidated
S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0)
Final stress
σ′f = σ′0 + Δσ (at mid-depth of the layer)
Overconsolidated, σ′f ≤ σ′p
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0)
Overconsolidated, σ′f > σ′p
S = H/(1 + e0)·[Cr·log₁₀(σ′p/σ′0) + Cc·log₁₀(σ′f/σ′p)]
Overconsolidation ratio
OCR = σ′p/σ′0
Time for consolidation
t = Tv·Hdr²/cv
Drainage path
Hdr = H/2 (double drainage), H (single drainage)
Time factors
U 50% → 0.197, 60% → 0.287, 70% → 0.403, 80% → 0.567, 90% → 0.848

Hydrostatic force

Pressure at depth
p = ρgh
Force on a vertical wall
F = ρg·hc·A
Centre of pressure
yp = yc + Ic/(ycA)
Rectangle
Ic = bH³/12

Pipe friction & head loss

Reynolds number
Re = V·D/ν = ρ·V·D/μ
Flow regime
laminar below Re ≈ 2000, turbulent above Re ≈ 4000
Mean velocity
V = Q/A, A = π·D²/4
Darcy–Weisbach
hf = f·(L/D)·V²/(2g)
Minor losses
hm = ΣK·V²/(2g)
Typical K values
entrance 0.5, exit 1.0, 90° bend ≈ 0.3
Pressure drop
Δp = ρ·g·hf
Two open reservoirs
Δz = (f·L/D + ΣK)·V²/(2g)
Free outlet
H = (1 + f·L/D + ΣK)·V²/(2g)

Open-channel flow (Manning)

Manning equation
V = (1/n)·R2/3·S1/2
Flow rate
Q = A·V
Hydraulic radius
R = A/P (P = wetted perimeter, free surface excluded)
Rectangle
A = b·y, P = b + 2y
Trapezoid (side slope z:1)
A = (b + z·y)·y, P = b + 2y·√(1 + z²)
Circular pipe, full or half full
R = D/4
Required slope
S = (n·Q/(A·R2/3))²

Pumps & pump power

Hydraulic power
Ph = ρ·g·Q·H = Q·Δp
Shaft power
Pshaft = Ph/ηpump
Electrical power
Pel = Pshaft/ηmotor
Pump head
H = Δz + Δp/(ρ·g) + hL
System losses
hL = (f·L/D + ΣK)·V²/(2g)

Time value of money

Future value
FV = PV·(1 + i)n
Present value
PV = FV/(1 + i)n
Several periods per year
i = r/m, N = m·n
Annuity, present value
PV = PMT·[1 − (1 + i)−n]/i
Annuity, future value
FV = PMT·[(1 + i)n − 1]/i

Method

  1. Draw a timeline with every cash flow and its timing.
  2. Match the rate to the period: a monthly rate for monthly payments.
  3. Use FV = PV·(1 + i)ⁿ for single amounts and the annuity formulas for equal payments.
  4. Check the sign and the order of magnitude of the answer.

NPV & IRR

Net present value
NPV = −C0 + Σ CFt/(1 + r)t
Equal cash flows
NPV = −C0 + CF·[1 − (1 + r)−n]/r
Internal rate of return
the r at which NPV = 0
Decision
accept when NPV > 0 (or IRR > required return)

Method

  1. List all cash flows with their year; the investment at year 0 is negative.
  2. Discount each cash flow: CFt/(1 + r)t.
  3. Add them up to get the NPV. Positive means the project earns more than r.
  4. For the IRR, find the rate that makes NPV zero by trial or interpolation.

Normal distribution

z-score
z = (x − μ)/σ
Below x
P(X < x) = Φ(z)
Above x
P(X > x) = 1 − Φ(z)
Between
Φ(z2) − Φ(z1)
Percentile
x = μ + z·σ

Method

  1. Convert the value to a z-score: z = (x − μ)/σ.
  2. Look up Φ(z), the area to the left of z.
  3. For the area to the right use 1 − Φ(z); for an interval subtract the two left areas.
  4. For a percentile, work backwards: find z for the area, then x = μ + z·σ.

2Practice problems

1.Beam support reactionsMedium
P1​ = 30 kNP2​ = 30 kNABRA​RB​ = ?4 m3 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 = 30 kN at 4 mP2 = 30 kN at 7 m
RB = kN
2.Beam support reactionsHard
w = 6 kN/mP = 30 kNABRA​RB​ = ?7 m1 m

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

L = 8 mP = 30 kN at 7 mw = 6 kN/m from 0 to 7 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB45 kN6 m2 m4 m

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

span = 6 mheight = 4 mB is 2 m from Avertical load = 45 kN
FBC = kN
4.Truss: method of jointsHard
ABCDEFGH20 kN30 kN15 kN15 kN4 × 4 m3 m

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

D: 20 kN ↓F: 30 kN →G: 15 kN ↓H: 15 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 BG
  13. 13member DG
5.Shear force & bending momentMedium
w = 5 kN/mABsection2.5 m2.5 m

Find the bending moment Mx at the section x = 2.5 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 = 2.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 3 kN/mP = 40 kNABsection1 m6 m1 m

Find the bending moment Mx at the section x = 7 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 40 kN at 1 mw = 3 kN/m from 0 to 8 mx = 7 m
Mx = kN·m
7.Beam deflectionMedium
P = 5 kNABδ4.5 m0.5 m

A cantilever of length L is fixed at A and carries a point load P at a distance a = 4.5 m from A. Find the deflection δB at the free end B.

P = 5 kNa = 4.5 mL = 5 mE = 200 GPa (steel)I = 84 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
w = 12 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 = 12 kN/mL = 5 mE = 70 GPa (aluminium)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 5 m20 × 80 mmcross-section

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

L = 5 mE = 70 GPa (aluminium)b × h = 20 × 80 mm
Pcr = kN
10.Column bucklingHard
PL = 1.5 md = 50 mmcross-section

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

L = 1.5 mE = 200 GPa (steel)d = 50 mm
σcr = MPa
11.Centroid & second moment of areaMedium
xD = 190d = 170dimensions in mm

A circular tube has outside diameter D = 190 mm and inside diameter d = 170 mm. Find its radius of gyration r about the horizontal centroidal axis.

D = 190 mmd = 170 mm
r = mm
12.Centroid & second moment of areaHard
140170102901612xdimensions in mm

A welded I-section has a top flange 140 × 10 mm, a web 290 mm high and 12 mm thick, and a bottom flange 170 × 16 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 140 × 10 mmweb: 12 × 290 mmbottom flange: 170 × 16 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 19 kN/m³10 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 = 15.5 kN/m³sand: γsat = 19 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 20.5 kN/m³5 mclayγsat​ = 19 kN/m³8 mwater tableXz = 9 m

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

z = 9 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 19 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 40 kPasandclayCc​ = 0.4, Cr​ = 0.03e0​ = 0.6σ′0​ = 105 kPaOCR = 2.55 mwater table

A 5 m thick overconsolidated clay layer has Cc = 0.4, Cr = 0.03 and e₀ = 0.6. At its mid-depth the effective vertical stress is 105 kPa and the overconsolidation ratio is OCR = 2.5. A new building adds 40 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 5 mCc = 0.4Cr = 0.03e0 = 0.6σ′0 = 105 kPaOCR = 2.5Δσ = 40 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 3 mcv​ = 0.8 m²/year3 mimpervious rockwater table

A clay layer 3 m thick has a coefficient of consolidation cv = 0.8 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 60% average consolidation the time factor is Tv = 0.287. How many years t does the layer take to reach 60% consolidation?

H = 3 mcv = 0.8 m²/yearU = 60%Tv = 0.287single drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 2 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

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

A vertical rectangular gate 1 m wide sits in the wall of a tank of oil, with its top edge 2 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 2 mH = 2 mb = 1 mρ = 880 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 2.5 m/sD = 300 mmL = 1000 mf = 0.022

Water (ρ = 1000 kg/m³) flows at 2.5 m/s through a horizontal pipe, 1000 m long, with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.022 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 2.5 m/sL = 1000 mD = 300 mmf = 0.022ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 2Δz = 37 mL = 300 m, D = 200 mm, f = 0.0182× bend (K = 0.3)

Two open reservoirs are joined by a pipe 300 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.018. The water surface of the upper reservoir is 37 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 2 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 = 37 mL = 300 mD = 200 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 2Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 4 my = 0.8 mn = 0.022, S = 0.002

A rectangular clean earth channel is 4 m wide. Water flows uniformly 0.8 m deep. Manning n = 0.022 and the bed slope is S = 0.002. Find the flow rate Q in m³/s.

b = 4 my = 0.8 mn = 0.022S = 0.002
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 5 my = 2.3 m2 : 1n = 0.03, Q = 42 m³/s

A trapezoidal grass-lined earth channel with a bottom width of 5 m and side slopes of 2:1 (horizontal:vertical) must carry 42 m³/s in uniform flow at a depth of 2.3 m. Manning n = 0.03. Find the required bed slope S (in m/m).

Q = 42 m³/sb = 5 my = 2.3 mz = 2n = 0.03
S = m/m
23.Pumps & pump powerMedium
PQ = 40 L/sH = 12 m

In a test, a pump delivers 40 L/s of water (ρ = 1000 kg/m³) against a head of 12 m while its shaft takes 5.7 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 40 L/sH = 12 mPshaft = 5.7 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 15 L/sΔz = 7 mL = 200 m, D = 100 mm, f = 0.018, ΣK = 8

A pump moves 15 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 7 m higher. The pipe is 200 m long with an inside diameter of 100 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 pump efficiency is 75%. Find the shaft power Pshaft in kW.

Q = 15 L/sΔz = 7 mL = 200 mD = 100 mmf = 0.018ΣK = 8η = 75%
Pshaft = kW
25.Time value of moneyMedium
years0123…12€20 000FV = ?

You invest €20 000 at 7% per year with continuous compounding. Find the value FV after 12 years.

PV = €20 000r = 7%t = 12
FV = €
26.Time value of moneyHard
months0123…156A?AA€75 000

You want €75 000 in 13 years. You save the same amount at the end of every month in an account paying 4.2% per year, compounded monthly. Find the monthly deposit A.

FV = €75 0004.2% / 12N = 156
A = €
27.NPV & IRRMedium
years0123…9−400 00029 000+2%+2%…r = 10%, NPV = ?

A project costs €400 000 today. It generates €29 000 at the end of the first year, and the cash flow then grows by 2% per year forever. The cost of capital is 10%. Find the net present value NPV.

C0 = €400 000CF1 = €29 000g = 2%r = 10%
NPV = €
28.NPV & IRRHard
years0123−10 0007 5004 0005 500

A project costs €10 000 and returns €7 500, €4 000, €5 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −10 000CF1 = 7 500CF2 = 4 000CF3 = 5 500
IRR = %
29.Normal distributionMedium
750 g735.2 gX + Y?

X is normal with mean 250 g and standard deviation 4 g; Y is independent and normal with mean 500 g and standard deviation 9 g. Find the probability P that X + Y is more than 735.2 g. Round z to two decimals.

μX = 250, σX = 4μY = 500, σY = 9X + Y > 735.2 g
P =
30.Normal distributionHard
μ = 65x = ?25%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Find the value x below which 25% of them lie (the 25th percentile).

μ = 65σ = 10P = 25%
x = points

3Solutions

1.Beam support reactions

Answer: RB = 41.25 kN

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

P1​ = 30 kNP2​ = 30 kNABRA​RB​4 m3 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 = 30·4 + 30·7
RB = 330/8 = 41.25 kN
ΣFy = 0: RA = 60 − 41.25 = 18.75 kN

Answer

RB = 41.25 kN
2.Beam support reactions

Answer: RB = 44.63 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 = 6 kN/mP = 30 kNABRA​RB​7 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 = 6·7 = 42 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·8 = 30·7 + 6·7·3.5
RB = 357/8 = 44.63 kN
ΣFy = 0: RA = 72 − 44.63 = 27.38 kN

Answer

RB = 44.63 kN
3.Truss: method of joints

Answer: FBC = −21.21 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.

ABBCACACB45 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 45·2 → Cy = 15 kN
ΣFy = 0: Ay = 45 − 15 = 30 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 = 4/5.657 = 0.7071, cos γ = 4/5.657 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −15/0.7071 = −21.21 kN

Answer

FBC = −21.21 kN (compression)
4.Truss: method of joints

Answer: member CG

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

Joint C

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

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

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

AB: 44.17 kN (T), BC: 58.33 kN (T), CD: 58.33 kN (T), DE: 52.5 kN (T), FG: 44.17 kN (C), GH: 52.5 kN (C), AF: 17.71 kN (C), HE: 65.62 kN (C), BF: 10.63 kN (T), CG: 0, DH: 24.38 kN (T), BG: 17.71 kN (C), DG: 7.292 kN (C)

Answer

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

Answer: Mx = 15.63 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 = 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​ = 12.5section2.5 m2.5 m

Cut at x = 2.5 m and keep the left part

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

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 12.5·2.5 − 5·2.5·1.25 = 15.63 kN·m

Answer

Mx = 15.63 kN·m
6.Shear force & bending moment

Answer: Mx = 15.5 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 3·8 = 24 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 40·1 + 3·8·4
RB = 136/8 = 17 kN
ΣFy = 0: RA = 64 − 17 = 47 kN
w = 3 kN/mP = 40 kNABRA​ = 47RB​ = 17section1 m6 m1 m

Cut at x = 7 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 = 47·7 − 40·(7 − 1) − 3·7·3.5 = 15.5 kN·m

Answer

Mx = 15.5 kN·m
7.Beam deflection

Answer: δB = 10.55 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 = 5000 N, a = 4500 mm, L = 5000 mm
EI = 1.68 × 10¹³ N·mm²

Deflection at the free end

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

δP = Pa³/(3EI) = 9.04 mm
θP = Pa²/(2EI) = 0.003013 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 10.55 mm

Answer

δB = 10.55 mm
8.Beam deflection

Answer: Ireq = 100.4 × 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) = 5·12·5000⁴/(384·70000·13.89) = 1.004 × 10⁸ mm⁴
Ireq = 100.4 × 10⁶ mm⁴

Answer

Ireq = 100.4 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 5.895 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 = 80·20³/12 = 53333 mm⁴

Effective length

KL = 0.5·5000 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·53333/2500² = 5895 N = 5.895 kN

Answer

Pcr = 5.895 kN
10.Column buckling

Answer: σcr = 34.27 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·50⁴/64 = 306796 mm⁴

Radius of gyration and slenderness

A = 1963 mm²
r = √(I/A) = √(306796/1963) = 12.5 mm
KL = 2·1500 = 3000 mm
KL/r = 3000/12.5 = 240

Critical stress

σcr = π²E/(KL/r)² = π²·200000/240² = 34.27 MPa

Answer

σcr = 34.27 MPa
11.Centroid & second moment of area

Answer: r = 63.74 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

A = π(D² − d²)/4 = 5655 mm²
I = π(D⁴ − d⁴)/64 = 2.297 × 10⁷ mm⁴

Radius of gyration

r = √(I/A) = √(2.297 × 10⁷/5655) = 63.74 mm

Answer

r = 63.74 mm
12.Centroid & second moment of area

Answer: Ix = 114 × 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 = 1400 mm², y = 311 mm
web: A = 3480 mm², y = 161 mm
bottom flange: A = 2720 mm², y = 8 mm

Centroid

ȳ = (1400·311 + 3480·161 + 2720·8)/7600 = 133.9 mm

Parallel-axis theorem

top flange: 140·10³/12 + 1400·177.1² = 4.393 × 10⁷ mm⁴
web: 12·290³/12 + 3480·27.13² = 2.695 × 10⁷ mm⁴
bottom flange: 170·16³/12 + 2720·125.9² = 4.315 × 10⁷ mm⁴
Ix = 4.393 × 10⁷ + 2.695 × 10⁷ + 4.315 × 10⁷
Ix = 1.14 × 10⁸ mm⁴ = 114 × 10⁶ mm⁴

Answer

Ix = 114 × 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′ = 106.1 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·3 + γsat,sand·2 + γsat,clay·4
σ = 16·3 + 20.5·2 + 19·4 = 165 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 = 165 − 58.86 = 106.1 kPa

Answer

σ′ = 106.1 kPa
15.Consolidation settlement

Answer: S = 13.14 mm

Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.

Preconsolidation pressure

σ′p = OCR·σ′0 = 2.5·105 = 262.5 kPa

Compare with the preconsolidation pressure

σ′f = 105 + 40 = 145 kPa ≤ 262.5 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.03·5/(1 + 0.6)·log₁₀(145/105) = 13.14 mm

Answer

S = 13.14 mm
16.Consolidation settlement

Answer: t = 3.229 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 = 3 m

Time

t = Tv·Hdr²/cv = 0.287·3²/0.8 = 3.229 years

Answer

t = 3.229 years
17.Hydrostatic force

Answer: F = 88.29 kN

Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.

Centroid depth and area

yc = d + H/2 = 2 + 2/2 = 3 m
A = H·b = 2·1.5 = 3 m²
gated = 2 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3·3 = 88.29 kN

Answer

F = 88.29 kN
18.Hydrostatic force

Answer: ycp = 3.111 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 + 2/2 = 3 m
A = H·b = 2·1 = 2 m²
gated = 2 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·3·2 = 51.8 kN

Centre of pressure

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

Ic = b·H³/12 = 1·2³/12 = 0.6667 m⁴
ycp = yc + Ic/(yc·A) = 3 + 0.6667/(3·2) = 3.111 m

Answer

ycp = 3.111 m
19.Pipe friction & head loss

Answer: Δp = 229.2 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) = 0.022·(1000/0.3)·2.5²/(2·9.81) = 23.36 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 = 1000·9.81·23.36 = 229167 Pa = 229.2 kPa

Answer

Δp = 229.2 kPa
20.Pipe friction & head loss

Answer: Q = 151.8 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 = 0.018·300/0.2 = 27
ΣK = 0.5 + 2·0.3 + 2 + 1.0 = 4.1

Energy equation

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

37 = (27 + 4.1)·V²/(2·9.81)
V = √(2·9.81·37/31.1) = 4.831 m/s

Flow rate

Q = V·π·D²/4 = 4.831·0.03142 = 0.1518 m³/s = 151.8 L/s

Answer

Q = 151.8 L/s
21.Open-channel flow (Manning)

Answer: Q = 4.479 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·y = 4·0.8 = 3.2 m²
P = b + 2y = 4 + 2·0.8 = 5.6 m
R = A/P = 0.5714 m

Velocity

V = (1/0.022)·0.57142/3·0.0021/2 = 1.4 m/s

Flow rate

Q = A·V = 3.2·1.4 = 4.479 m³/s

Answer

Q = 4.479 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.001994 m/m

Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.

Geometry

A = (b + z·y)·y = (5 + 2·2.3)·2.3 = 22.08 m²
P = b + 2y·√(1 + z²) = 5 + 2·2.3·√(1 + 2²) = 15.29 m
R = A/P = 1.444 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.03·42/(22.08·1.278) = 0.04466
S = 0.04466² = 0.001994

Answer

S = 0.001994

That is a fall of 1.994 m per kilometre.

23.Pumps & pump power

Answer: η = 82.61 %

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 = 1000·9.81·0.04·12 = 4.709 kW

Efficiency

η = Ph/Pshaft = 4.709/5.7 = 82.61%

Answer

η = 82.61%
24.Pumps & pump power

Answer: Pshaft = 2.978 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 = 0.015/0.007854 = 1.91 m/s
V²/(2g) = 0.1859 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (36 + 8)·0.1859 = 8.18 m

Pump head

H = Δz + hL = 7 + 8.18 = 15.18 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.015·15.18/0.75 = 2.978 kW

Answer

Pshaft = 2.978 kW
25.Time value of money

Answer: FV = 46327 €

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

Exponent

r·t = 0.07·12 = 0.84
e0.84 = 2.316

Future value

FV = 20 000·2.316 = €46 327.34

Answer

FV = €46 327.34
26.Time value of money

Answer: A = 362.2 €

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 = 0.042/12 = 0.0035
N = 12·13 = 156

Deposit

A = FV·i/((1 + i)N − 1) = 75 000·0.0035/(1.725 − 1) = €362.22

Answer

A = €362.22
27.NPV & IRR

Answer: NPV = −37500 €

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

Value of the cash flows

PV = 29 000/(0.1 − 0.02) = 362 500.00

NPV

NPV = 362 500.00 − 400 000 = −€37 500.00

Answer

NPV = −€37 500.00

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

28.NPV & IRR

Answer: IRR = 34.88 %

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(30%) = 639.51
NPV(35%) = −14.23

Narrow down

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

IRR ≈ 30 + 5·639.51/(639.51 − (−14.23)) = 34.89%
exact: NPV(34.88%) = 0 → IRR = 34.88%

Answer

IRR = 34.88%
29.Normal distribution

Answer: P = 0.9332

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 = 750 g, σ = √(4² + 9²) = 9.849 g

Standardise

z = (735.2 − 750)/9.849 = −1.5

Upper tail

P = 1 − Φ(−1.5) = 1 − 0.06681 = 0.9332

Answer

P = 0.9332
30.Normal distribution

Answer: x = 58.26 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) = 0.25 → z = −0.6745

Back to x

x = 65 + −0.6745·10 = 58.26 points

Answer

x = 58.26 points

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