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​ = 40 kNP2​ = 20 kNABRA​ = ?RB​1.5 m1 m1.5 m

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

L = 4 mP1 = 40 kN at 1.5 mP2 = 20 kN at 2.5 m
RA = kN
2.Beam support reactionsHard
w = 6 kN/mP = 35 kNABRA​RB​ = ?1 m2 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 mP = 35 kN at 1 mw = 6 kN/m from 3 to 7 m
RB = kN
3.Truss: method of jointsMedium
ABCDEFGH35 kN40 kN30 kN20 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.

B: 35 kN ↓D: 40 kN ↓F: 30 kN ↓H: 20 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
4.Truss: method of jointsHard
ABCDEFGH30 kN10 kN15 kN10 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.

B: 30 kN ↓C: 10 kN ↓D: 15 kN ↓F: 10 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
5.Shear force & bending momentMedium
w = 8 kN/mABsection1 m5 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 = 6 mw = 8 kN/m from 0 to 6 mx = 1 m
Mx = kN·m
6.Shear force & bending momentHard
5 kN/m10 kN10 kNABCDEFG1 m1 m1 m1 m1 m1 m

The marks A to G split the beam into six equal parts. At which mark is the bending moment largest in size, sagging or hogging? Click it in the diagram.

10 kN @ 6 m10 kN @ 1 m5 kN/m, 0–4 m
  1. 1A (x = 0 m)
  2. 2B (x = 1 m)
  3. 3C (x = 2 m)
  4. 4D (x = 3 m)
  5. 5E (x = 4 m)
  6. 6F (x = 5 m)
  7. 7G (x = 6 m)
7.Beam deflectionMedium
w = 20 kN/mδL = 8 m

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

w = 20 kN/mL = 8 mE = 200 GPa (steel)I = 120 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 10 kN/mP = 2 kNδL = 4 m

A simply supported beam carries a uniformly distributed load w and a point load P at midspan. Using superposition, find the midspan deflection δmax.

P = 2 kNw = 10 kN/mL = 4 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 3 m25 × 80 mmcross-section

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

L = 3 mE = 200 GPa (steel)b × h = 25 × 80 mm
Pcr = kN
10.Column bucklingHard
P = 65 kNL = 2 md = ?cross-section

A solid round column of length L made of aluminium is pinned at both ends. It must carry 65 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 65 kNn = 2L = 2 mE = 70 GPa (aluminium)
d = mm
11.Centroid & second moment of areaMedium
1002516010xdimensions in mm

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

bf = 100 mmtf = 25 mmtw = 10 mmhw = 160 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1801020020xsagging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 50 MPa in tension and 100 MPa in compression. Find the largest sagging bending moment Mallow the beam can carry.

bf = 180 mmtf = 10 mmtw = 20 mmhw = 200 mmσt,allow = 50 MPaσc,allow = 100 MPa
Mallow = kN·m
13.Effective stress in soilMedium
sandγd​ = 17 kN/m³γsat​ = 19.5 kN/m³10 mwater tableXz = 10 m

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

z = 10 mzw = 3 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 19.5 kN/m³3 mclayγsat​ = 18 kN/m³7 mwater tableXz = 6.5 m

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

z = 6.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19.5 kN/m³clay: γsat = 18 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 20 kPasandclayCc​ = 0.4, Cr​ = 0.05e0​ = 0.9σ′0​ = 105 kPaOCR = 32.5 mwater table

A 2.5 m thick overconsolidated clay layer has Cc = 0.4, Cr = 0.05 and e₀ = 0.9. At its mid-depth the effective vertical stress is 105 kPa and the overconsolidation ratio is OCR = 3. A new building adds 20 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2.5 mCc = 0.4Cr = 0.05e0 = 0.9σ′0 = 105 kPaOCR = 3Δσ = 20 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 7 mcv​ = 2.5 m²/year7 mimpervious rockwater table

A clay layer 7 m thick has a coefficient of consolidation cv = 2.5 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 = 7 mcv = 2.5 m²/yearU = 90%Tv = 0.848single drainage
t = years
17.Hydrostatic forceMedium
gated = 4 mH = 1.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 1.5 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2 mH = 1 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of seawater, with its top edge 2 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 2 mH = 1 mb = 3 mρ = 1025 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 1.7 m/sD = 200 mmL = 400 mf = 0.015

Water (ρ = 1000 kg/m³) flows at 1.7 m/s through a horizontal pipe, 400 m long, with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1.7 m/sL = 400 mD = 200 mmf = 0.015ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 5free outletH = ?L = 100 m, D = 200 mm, f = 0.023× bend (K = 0.3)

A pipe 100 m long with an inside diameter of 200 mm (Darcy friction factor f = 0.02) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each) and a valve (K = 5). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 40 L/s?

Q = 40 L/sL = 100 mD = 200 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5
H = m
21.Open-channel flow (Manning)Medium
D = 450 mmn = 0.013, S = 0.0005

A concrete storm sewer with an inside diameter of 450 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.0005. Find the flow rate Q in m³/s.

D = 450 mmn = 0.013S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 450 mmn = 0.013, V = 0.75 m/s

A concrete sewer with an inside diameter of 450 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.75 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 450 mmn = 0.013V = 0.75 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 100 L/sH = 78 m

A pump delivers 100 L/s of water (ρ = 1000 kg/m³) against a head of 78 m. The pump efficiency is 65% and the electric motor driving it has an efficiency of 92%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 100 L/sH = 78 mηpump = 65%ηmotor = 92%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
250 kPa (gauge)PQ = 80 L/sΔz = 5 mL = 300 m, D = 250 mm, f = 0.022, ΣK = 4

A pump moves 80 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 5 m higher. The pipe is 300 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 4 (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 250 kPa. Find the head H the pump must add.

Q = 80 L/sΔz = 5 mL = 300 mD = 250 mmf = 0.022ΣK = 4ptank = 250 kPa
H = m
25.Time value of moneyMedium
years01234PV = ?€5 000

You need €5 000 in 4 years. An account pays 2% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €5 0002% / 4n = 4
PV = €
26.Time value of moneyHard
months0123…264€100€100€100FV = ?

You save €100 at the end of every month for 22 years. The account pays 7.2% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €1007.2% / 12N = 264
FV = €
27.NPV & IRRMedium
years01234−45 00020 00016 00011 00017 000

An investment of €45 000 gives these cash flows at the end of years 1 to 4: €20 000, €16 000, €11 000, €17 000. The cost of capital is 7.000000000000001%. Find the net present value NPV.

r = 7.000000000000001%CF0 = −45 000CF1 = 20 000CF2 = 16 000CF3 = 11 000CF4 = 17 000
NPV = €
28.NPV & IRRHard
years012−10 0007 5005 000

A project costs €10 000 and returns €7 500, €5 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −10 000CF1 = 7 500CF2 = 5 000
IRR = %
29.Normal distributionMedium
85112P = ?

The IQ scores are normally distributed with mean 100 points and standard deviation 15 points. What fraction lies between 85 and 112 points? Give P as a decimal.

μ = 100σ = 15x1 = 85x2 = 112
P =
30.Normal distributionHard
0.05 mm0D − d?

Hole diameters D are normal with mean 25.05 mm and standard deviation 0.01 mm. Shaft diameters d are independent and normal with mean 25 mm and standard deviation 0.02 mm. A randomly chosen shaft fits when D − d > 0. Find the probability P that it fits. Round z to two decimals.

hole: μ = 25.05 mm, σ = 0.01 mmshaft: μ = 25 mm, σ = 0.02 mm
P =

3Solutions

1.Beam support reactions

Answer: RA = 32.5 kN

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

P1​ = 40 kNP2​ = 20 kNABRA​RB​1.5 m1 m1.5 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·4 = 40·1.5 + 20·2.5
RB = 110/4 = 27.5 kN
ΣFy = 0: RA = 60 − 27.5 = 32.5 kN

Answer

RA = 32.5 kN
2.Beam support reactions

Answer: RB = 19.38 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 = 35 kNABRA​RB​1 m2 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.

UDL resultant: W = w·ℓ = 6·4 = 24 kN, acting at x̄ = 5 m
ΣMA = 0: RB·8 = 35·1 + 6·4·5
RB = 155/8 = 19.38 kN
ΣFy = 0: RA = 59 − 19.38 = 39.63 kN

Answer

RB = 19.38 kN
3.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: 85 kN (T), BC: 83.33 kN (T), CD: 83.33 kN (T), DE: 81.67 kN (T), FG: 85 kN (C), GH: 81.67 kN (C), AF: 106.3 kN (C), HE: 102.1 kN (C), BF: 33.75 kN (T), CG: 0, DH: 41.25 kN (T), BG: 2.083 kN (T), DG: 2.083 kN (C)

Answer

Zero-force member: CG
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 G

FG and GH 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: 49.17 kN (T), BC: 49.17 kN (T), CD: 34.17 kN (T), DE: 34.17 kN (T), FG: 48.33 kN (C), GH: 48.33 kN (C), AF: 48.96 kN (C), HE: 42.71 kN (C), BF: 30 kN (T), CG: 0, DH: 15 kN (T), FC: 1.042 kN (C), HC: 17.71 kN (T)

Answer

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

Answer: Mx = 20 kN·m

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

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 8·6 = 48 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 8·6·3
RB = 144/6 = 24 kN
ΣFy = 0: RA = 48 − 24 = 24 kN
w = 8 kN/mABRA​ = 24RB​ = 24section1 m5 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 = 24·1 − 8·1·0.5 = 20 kN·m

Answer

Mx = 20 kN·m
6.Shear force & bending moment

Answer: E (x = 4 m)

Largest bending moment: M changes slope wherever the shear force changes, so its peaks sit where the shear force crosses zero: under a point load, inside a distributed load, or over a support of an overhang. At a fixed support of a cantilever the moment is largest at the wall. Compare the size of M at those places, sagging or hogging.

Support reactions

Take moments about one support, then use the vertical force balance.

R1 = 12.5 kN, R2 = 27.5 kN

Bending moment at every mark

Sum the moments of all forces on one side of the cut. Sagging is positive, hogging negative.

MA = 0, MB = 10, MC = 5, MD = −5, ME = −20 kN·m, MF = −10, MG = 0

Answer

Mark E: ME = −20 kN·m
7.Beam deflection

Answer: δmax = 44.44 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 = 20 N/mm, L = 8000 mm
EI = 2.4 × 10¹³ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·20·8000⁴/(384·2.4 × 10¹³) = 44.44 mm

Answer

δmax = 44.44 mm
8.Beam deflection

Answer: δmax = 15 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 = 2000 N, w = 10 N/mm, L = 4000 mm, EI = 2.4 × 10¹² N·mm²

Each load on its own

δP = PL³/(48EI) = 2000·4000³/(48·2.4 × 10¹²) = 1.111 mm
δw = 5wL⁴/(384EI) = 5·10·4000⁴/(384·2.4 × 10¹²) = 13.89 mm

Add them

δmax = 1.111 + 13.89 = 15 mm

Answer

δmax = 15 mm
9.Column buckling

Answer: Pcr = 22.85 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 = 80·25³/12 = 104167 mm⁴

Effective length

KL = 1·3000 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·104167/3000² = 22846 N = 22.85 kN

Answer

Pcr = 22.85 kN
10.Column buckling

Answer: d = 62.58 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 = 2·65000 = 130000 N
KL = 1·2000 = 2000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·130000·2000²/(π³·70000))^(1/4) = 62.58 mm

Answer

d = 62.58 mm

Check: the slenderness KL/r is 127.8, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 11.89 × 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 = 100·25 = 2500 mm², yf = 160 + 25/2 = 172.5 mm
web: Aw = 10·160 = 1600 mm², yw = 160/2 = 80 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2500·172.5 + 1600·80)/4100 = 136.4 mm

Parallel-axis theorem

flange: 100·25³/12 + 2500·(172.5 − 136.4)² = 3.388 × 10⁶ mm⁴
web: 10·160³/12 + 1600·(80 − 136.4)² = 8.503 × 10⁶ mm⁴
Ix = 3.388 × 10⁶ + 8.503 × 10⁶ = 1.189 × 10⁷ mm⁴ = 11.89 × 10⁶ mm⁴

Answer

Ix = 11.89 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 10.2 kN·m

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.

Centroid

ȳ = (1800·205 + 4000·100)/5800 = 132.6 mm
top edge: c = 210 − 132.6 = 77.41 mm

Second moment of area

I = 180·10³/12 + 1800·72.41² + 20·200³/12 + 4000·32.59² = 2.703 × 10⁷ mm⁴

Moment allowed by each edge

Sagging: the top is in compression, the bottom in tension.

top edge: M = 100·2.703 × 10⁷/77.41 = 34.92 kN·m
bottom edge: M = 50·2.703 × 10⁷/132.6 = 10.2 kN·m

Governing value

Mallow = min = 10.2 kN·m (bottom edge)

Answer

Mallow = 10.2 kN·m
13.Effective stress in soil

Answer: σ′ = 118.8 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) = 17·3 + 19.5·7 = 187.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·7 = 68.67 kPa

Effective stress

σ′ = σ − u = 187.5 − 68.67 = 118.8 kPa

Answer

σ′ = 118.8 kPa
14.Effective stress in soil

Answer: σ′ = 64.04 kPa

Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).

Total stress

Add the weight of each soil band above X. Above the water table use the dry unit weight, below it the saturated one.

σ = γd·1 + γsat,sand·2 + γsat,clay·3.5
σ = 16·1 + 19.5·2 + 18·3.5 = 118 kPa

Pore water pressure

Water pressure grows with depth below the water table.

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

Effective stress

σ′ = σ − u = 118 − 53.96 = 64.04 kPa

Answer

σ′ = 64.04 kPa
15.Consolidation settlement

Answer: S = 4.982 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 = 3·105 = 315 kPa

Compare with the preconsolidation pressure

σ′f = 105 + 20 = 125 kPa ≤ 315 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·2.5/(1 + 0.9)·log₁₀(125/105) = 4.982 mm

Answer

S = 4.982 mm
16.Consolidation settlement

Answer: t = 16.62 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 = 7 m

Time

t = Tv·Hdr²/cv = 0.848·7²/2.5 = 16.62 years

Answer

t = 16.62 years
17.Hydrostatic force

Answer: F = 139.8 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 + 1.5/2 = 4.75 m
A = H·b = 1.5·2 = 3 m²
gated = 4 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·4.75·3 = 139.8 kN

Answer

F = 139.8 kN
18.Hydrostatic force

Answer: ycp = 2.533 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 + 1/2 = 2.5 m
A = H·b = 1·3 = 3 m²
gated = 2 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·2.5·3 = 75.41 kN

Centre of pressure

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

Ic = b·H³/12 = 3·1³/12 = 0.25 m⁴
ycp = yc + Ic/(yc·A) = 2.5 + 0.25/(2.5·3) = 2.533 m

Answer

ycp = 2.533 m
19.Pipe friction & head loss

Answer: Δp = 43.35 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) = 0.015·(400/0.2)·1.7²/(2·9.81) = 4.419 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 = 1000·9.81·4.419 = 43350 Pa = 43.35 kPa

Answer

Δp = 43.35 kPa
20.Pipe friction & head loss

Answer: H = 1.438 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 = 0.04/0.03142 = 1.273 m/s
V²/(2g) = 0.08263 m

Loss coefficients

f·L/D = 0.02·100/0.2 = 10
ΣK = 0.5 + 3·0.3 + 5 = 6.4

Energy equation

The outlet jet still carries its velocity head; it is not a loss but it has to be supplied.

H = (1 + 10 + 6.4)·0.08263 = 1.438 m

Answer

H = 1.438 m
21.Open-channel flow (Manning)

Answer: Q = 0.06375 m³/s

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

Geometry

A = 0.159 m², R = D/4 = 0.1125 m

Velocity

V = (1/0.013)·0.11252/3·0.00051/2 = 0.4008 m/s

Flow rate

Q = A·V = 0.159·0.4008 = 0.06375 m³/s

Answer

Q = 0.06375 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.00175 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.

Hydraulic radius

R = D/4 = 0.45/4 = 0.1125 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.75/0.233)² = 0.00175

Answer

S = 0.00175

That is a fall of 1.75 m per kilometre.

23.Pumps & pump power

Answer: Pel = 128 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 = 1000·9.81·0.1·78 = 76.52 kW

Shaft power

Pshaft = 76.52/0.65 = 117.7 kW

Electrical power

Pel = 117.7/0.92 = 128 kW

Answer

Pel = 128 kW
24.Pumps & pump power

Answer: H = 34.6 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 = 0.08/0.04909 = 1.63 m/s
V²/(2g) = 0.1354 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (26.4 + 4)·0.1354 = 4.115 m

Pressure head

p/(ρ·g) = 250000/(1000·9.81) = 25.48 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 5 + 25.48 + 4.115 = 34.6 m

Answer

H = 34.6 m
25.Time value of money

Answer: PV = 4617 €

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 = 0.02/4 = 0.005
N = 4·4 = 16

Present value

PV = FV/(1 + i)N = 5 000/1.083 = €4 616.50

Answer

PV = €4 616.50
26.Time value of money

Answer: FV = 64190 €

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 = 0.07200000000000001/12 = 0.006
N = 12·22 = 264

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 100·(4.851 − 1)/0.006 = €64 189.97

Answer

FV = €64 189.97

You paid in €26 400 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = 9615 €

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 each cash flow

CF0 = −45 000
CF1/(1 + 0.07)1 = 20 000/1.07 = 18 691.59
CF2/(1 + 0.07)2 = 16 000/1.145 = 13 975.02
CF3/(1 + 0.07)3 = 11 000/1.225 = 8 979.28
CF4/(1 + 0.07)4 = 17 000/1.311 = 12 969.22

Add them up

NPV = €9 615.10

Answer

NPV = €9 615.10

NPV is positive, so the project earns more than the required return.

28.NPV & IRR

Answer: IRR = 17.54 %

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(15%) = 302.46
NPV(20%) = −277.78

Narrow down

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

IRR ≈ 15 + 5·302.46/(302.46 − (−277.78)) = 17.61%
exact: NPV(17.54%) = 0 → IRR = 17.54%

Answer

IRR = 17.54%
29.Normal distribution

Answer: P = 0.6295

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 = (85 − 100)/15 = −1
z₂ = (112 − 100)/15 = 0.8

Area between

P = Φ(0.8) − Φ(−1) = 0.7881 − 0.1587 = 0.6295

Answer

P = 0.6295
30.Normal distribution

Answer: P = 0.9875

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 difference

μ = 25.05 − 25 = 0.05 mm, σ = 0.02236 mm

Standardise

z = (0 − 0.05)/0.02236 = −2.24

Probability

P = 1 − Φ(−2.24) = 0.9875

Answer

P = 0.9875

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