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​ = 10 kNP2​ = 30 kNABRA​ = ?RB​1.5 m2 m1.5 m

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

L = 5 mP1 = 10 kN at 1.5 mP2 = 30 kN at 3.5 m
RA = kN
2.Beam support reactionsHard
w = 4 kN/mP = 25 kNABRA​RB​ = ?1 m2 m1 m

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

L = 4 mP = 25 kN at 1 mw = 4 kN/m from 0 to 3 m
RB = kN
3.Truss: method of jointsMedium
ABCDEFGH35 kN25 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.

D: 35 kN ↓G: 25 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
ABBCACACB25 kN20 kN5 m4 m3 m

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

span = 5 mheight = 3 mB is 4 m from Avertical load = 25 kNhorizontal load = 20 kN ←
FAC = kN
5.Shear force & bending momentMedium
w = 10 kN/mABsection0.5 m4.5 m

Find the bending moment Mx at the section x = 0.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mw = 10 kN/m from 0 to 5 mx = 0.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 5 kN/mABC6 m2 m

The beam rests on a pin at A and a roller at B and overhangs B by 2 m to the free end C. A uniformly distributed load w acts over the whole length A–C. Find the maximum sagging bending moment Mmax between the supports.

L = 8 mw = 5 kN/m from 0 to 8 msupports at x = 0 and x = 6 m
Mmax = kN·m
7.Beam deflectionMedium
w = 4 kN/mδL = 2.5 m

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

w = 4 kN/mL = 2.5 mE = 11 GPa (timber)I = 36 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
P = 60 kNAB4 m4 m

A propped cantilever is fixed at A and simply supported (propped) at B. It carries a point load P at midspan. EI is constant. Find the size of the bending moment MA at the fixed end.

L = 8 mP = 60 kN at 4 m
MA = kN·m
9.Column bucklingMedium
PL = 6 md = 30 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 = 6 mE = 70 GPa (aluminium)d = 30 mm
Pcr = kN
10.Column bucklingHard
P = 25 kNL = 3 md = ?cross-section

A solid round column of length L made of steel is fixed at both ends. It must carry 25 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 25 kNn = 2L = 3 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
2103402210xdimensions in mm

A symmetric I-section has flanges 210 mm wide and 22 mm thick, an overall depth of 340 mm and a web 10 mm thick. Find its elastic section modulus Sx for bending about the horizontal centroidal axis x.

B = 210 mmH = 340 mmtf = 22 mmtw = 10 mm
Sx = × 10³ mm³
12.Centroid & second moment of areaHard
2801024012xM = 30 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 30 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 280 mmtf = 10 mmtw = 12 mmhw = 240 mmM = 30 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 18.5 kN/m³13 mwater tableXz = 13 m

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

z = 13 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 18.5 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 19.5 kN/m³4 mclayγsat​ = 18.5 kN/m³8 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 = 19.5 kN/m³clay: γsat = 18.5 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 180 kPasandclayCc​ = 0.25, Cr​ = 0.02e0​ = 0.6σ′0​ = 110 kPaσ′p​ = 200 kPa3 mwater table

A 3 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.02 and e₀ = 0.6. At its mid-depth the effective vertical stress is 110 kPa and the preconsolidation pressure is 200 kPa. A new building adds 180 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 3 mCc = 0.25Cr = 0.02e0 = 0.6σ′0 = 110 kPaσ′p = 200 kPaΔσ = 180 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 4 m4 mimpervious rockwater table

In a laboratory oedometer test, a clay specimen 19 mm thick, drained at the top and bottom, reaches 50% consolidation in 8 min. In the field the same clay forms a layer 4 m thick. It lies on impervious rock, with sand above it, so water drains out only at the top. How many days t does the field layer take to reach 50% consolidation?

hlab = 19 mmtlab = 8 minH = 4 mfield: single drainage
t = days
17.Hydrostatic forceMedium
gated = 2.5 mH = 3 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 2.5 m below the surface. Find the resultant hydrostatic force F on the gate.

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

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 1.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1.5 mH = 1.5 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1.6 m/sD = 300 mmL = 500 mf = 0.02

Water (ρ = 1000 kg/m³) flows at 1.6 m/s through a horizontal pipe, 500 m long, with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.02 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1.6 m/sL = 500 mD = 300 mmf = 0.02ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 2Δz = ?L = 300 m, D = 300 mm, f = 0.0182× bend (K = 0.3)

Two open reservoirs are joined by a pipe 300 m long with an inside diameter of 300 mm and a Darcy friction factor f = 0.018. 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. What difference in water level Δz between the reservoirs gives a flow rate of 150 L/s?

Q = 150 L/sL = 300 mD = 300 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 2Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 4 my = 1.7 mn = 0.012, S = 0.005

A rectangular finished concrete channel is 4 m wide. Water flows uniformly 1.7 m deep. Manning n = 0.012 and the bed slope is S = 0.005. Find the flow rate Q in m³/s.

b = 4 my = 1.7 mn = 0.012S = 0.005
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 250 mmn = 0.013, V = 1.2 m/s

A concrete sewer with an inside diameter of 250 mm (Manning n = 0.013) must reach a self-cleansing velocity of 1.2 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 250 mmn = 0.013V = 1.2 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 60 L/sH = 72 m

A pump delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 72 m. The pump efficiency is 80% and the electric motor driving it has an efficiency of 90%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 60 L/sH = 72 mηpump = 80%ηmotor = 90%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
100 kPa (gauge)PQ = 75 L/sΔz = 34 mL = 400 m, D = 200 mm, f = 0.015, ΣK = 8

A pump moves 75 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 34 m higher. The pipe is 400 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 100 kPa. Find the head H the pump must add.

Q = 75 L/sΔz = 34 mL = 400 mD = 200 mmf = 0.015ΣK = 8ptank = 100 kPa
H = m
25.Time value of moneyMedium
years0123…8PV = ?€15 000

You need €15 000 in 8 years. An account pays 4% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €15 0004% / 12n = 8
PV = €
26.Time value of moneyHard
months0123…60€25 000A?AAA

A loan of €25 000 is repaid with equal monthly payments over 5 years. The interest rate is 2.4% per year, compounded monthly. Find the monthly payment A.

P = €25 0002.4% / 12N = 60
A = €
27.NPV & IRRMedium
years0123−45 00014 00015 00010 000

An investment of €45 000 gives these cash flows at the end of years 1 to 3: €14 000, €15 000, €10 000. The cost of capital is 6%. Find the net present value NPV.

r = 6%CF0 = −45 000CF1 = 14 000CF2 = 15 000CF3 = 10 000
NPV = €
28.NPV & IRRHard
years0123−40 00015 50028 00025 500

A project costs €40 000 and returns €15 500, €28 000, €25 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 15 500CF2 = 28 000CF3 = 25 500
IRR = %
29.Normal distributionMedium
105 s117.8 sX + Y?

X is normal with mean 60 s and standard deviation 5 s; Y is independent and normal with mean 45 s and standard deviation 4 s. Find the probability P that X + Y is more than 117.8 s. Round z to two decimals.

μX = 60, σX = 5μY = 45, σY = 4X + Y > 117.8 s
P =
30.Normal distributionHard
μ = 65x = ?10%

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

μ = 65σ = 10P = 10%
x = points

3Solutions

1.Beam support reactions

Answer: RA = 16 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​ = 10 kNP2​ = 30 kNABRA​RB​1.5 m2 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·5 = 10·1.5 + 30·3.5
RB = 120/5 = 24 kN
ΣFy = 0: RA = 40 − 24 = 16 kN

Answer

RA = 16 kN
2.Beam support reactions

Answer: RB = 10.75 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 = 4 kN/mP = 25 kNABRA​RB​1 m2 m1 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 4·3 = 12 kN, acting at x̄ = 1.5 m
ΣMA = 0: RB·4 = 25·1 + 4·3·1.5
RB = 43/4 = 10.75 kN
ΣFy = 0: RA = 37 − 10.75 = 26.25 kN

Answer

RB = 10.75 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: 21.25 kN (T), BC: 42.5 kN (T), CD: 42.5 kN (T), DE: 38.75 kN (T), FG: 21.25 kN (C), GH: 38.75 kN (C), AF: 30.05 kN (C), HE: 54.8 kN (C), BF: 21.25 kN (T), CG: 0, DH: 38.75 kN (T), BG: 30.05 kN (C), DG: 5.303 kN (C)

Answer

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

Answer: FAC = 2.667 kN

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

ABBCACACB25 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 25·4 − 20·3 → Cy = 8 kN
ΣFy = 0: Ay = 25 − 8 = 17 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 = 3/3.162 = 0.9487, cos γ = 1/3.162 = 0.3162
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −8/0.9487 = −8.433 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−8.433)·0.3162 = 2.667 kN

Answer

FAC = 2.667 kN (tension)
5.Shear force & bending moment

Answer: Mx = 11.25 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 = 10·5 = 50 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 10·5·2.5
RB = 125/5 = 25 kN
ΣFy = 0: RA = 50 − 25 = 25 kN
w = 10 kN/mABRA​ = 25RB​ = 25section0.5 m4.5 m

Cut at x = 0.5 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 = 25·0.5 − 10·0.5·0.25 = 11.25 kN·m

Answer

Mx = 11.25 kN·m
6.Shear force & bending moment

Answer: Mmax = 17.78 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut. Maximum moment: since dM/dx = V, the bending moment has its peak where the shear force passes through zero, either at a point load or inside a distributed load.

Support reactions

Equilibrium of the whole beam, including the load on the overhang.

UDL resultant: W = w·ℓ = 5·8 = 40 kN, acting at x̄ = 4 m
ΣMA = 0: RB·6 = 5·8·4
RB = 160/6 = 26.67 kN
ΣFy = 0: RA = 40 − 26.67 = 13.33 kN

Zero shear

RA − w·x0 = 0 → x0 = 13.33/5 = 2.667 m

Maximum sagging moment

Mmax = RA·x0 − w·x0²/2 = RA²/(2w) = 13.33²/(2·5) = 17.78 kN·m

Answer

Mmax = 17.78 kN·m
7.Beam deflection

Answer: δmax = 5.138 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 = 4 N/mm, L = 2500 mm
EI = 3.96 × 10¹¹ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·4·2500⁴/(384·3.96 × 10¹¹) = 5.138 mm

Answer

δmax = 5.138 mm
8.Beam deflection

Answer: MA = 90 kN·m

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). For a statically indeterminate beam, remove a redundant support and require the deflection there to be zero (compatibility).

Remove the prop

Without the prop the beam is a cantilever. Its free end would deflect under the load.

δload = P(L/2)²(3L − L/2)/(6EI) = 5PL³/(48EI)

Compatibility at the prop

The prop force RB alone lifts the free end by RBL³/(3EI). The prop holds B at zero deflection, so the two must cancel. EI cancels out.

RB·L³/(3EI) = 5PL³/(48EI) → RB = 5P/16 = 5·60/16 = 18.75 kN

Moment at the fixed end

Moments about A of the loads and the prop force.

MA = P·L/2 − RB·L = 240 − 150 = 90 kN·m

Answer

MA = 90 kN·m
9.Column buckling

Answer: Pcr = 3.052 kN

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

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·30⁴/64 = 39761 mm⁴

Effective length

KL = 0.5·6000 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·39761/3000² = 3052 N = 3.052 kN

Answer

Pcr = 3.052 kN
10.Column buckling

Answer: d = 32.83 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 = 2·25000 = 50000 N
KL = 0.5·3000 = 1500 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·50000·1500²/(π³·200000))^(1/4) = 32.83 mm

Answer

d = 32.83 mm

Check: the slenderness KL/r is 182.8, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Sx = 1503 × 10³ mm³

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.

Outer rectangle minus the two side cut-outs

Both cut-outs together are (B − tw) wide and hw = H − 2tf high, and share the axis x.

hw = 340 − 2·22 = 296 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (210·340³ − 200·296³)/12
Ix = 2.556 × 10⁸ mm⁴

Section modulus

c = H/2 = 170 mm
Sx = I/c = 2.556 × 10⁸/170
Sx = 1.503 × 10⁶ mm³ = 1503 × 10³ mm³

Answer

Sx = 1503 × 10³ mm³
12.Centroid & second moment of area

Answer: σbottom = 151.2 MPa

Composite areas: split the section into rectangles. The centroid is the area-weighted average ȳ = ΣAᵢyᵢ/ΣAᵢ. The second moment of area about the centroidal axis adds each part’s own bh³/12 and its parallel-axis term A·d², where d is the distance from the part’s centroid to the overall centroid. Bending stress is σ = M·y/I.

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 280·10 = 2800 mm², yf = 240 + 10/2 = 245 mm
web: Aw = 12·240 = 2880 mm², yw = 240/2 = 120 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2800·245 + 2880·120)/5680 = 181.6 mm

Parallel-axis theorem

flange: 280·10³/12 + 2800·(245 − 181.6)² = 1.127 × 10⁷ mm⁴
web: 12·240³/12 + 2880·(120 − 181.6)² = 2.476 × 10⁷ mm⁴
Ix = 1.127 × 10⁷ + 2.476 × 10⁷ = 3.603 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 181.6 mm
σ = M·y/I = 3 × 10⁷·181.6/3.603 × 10⁷ = 151.2 MPa

Answer

σbottom = 151.2 MPa
13.Effective stress in soil

Answer: u = 117.7 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) = 9.81·12 = 117.7 kPa

Answer

u = 117.7 kPa
14.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
15.Consolidation settlement

Answer: S = 85.38 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 = 110 + 180 = 290 kPa > 200 kPa

Settlement

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

S = 0.02·3/(1 + 0.6)·log₁₀(200/110) + 0.25·3/(1 + 0.6)·log₁₀(290/200)
S = 9.736 + 75.64 = 85.38 mm

Answer

S = 85.38 mm
16.Consolidation settlement

Answer: t = 984.9 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 = 19/2 = 9.5 mm = 0.0095 m
Hdr,field = 4 m

Scale the time

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

tfield = 8·(4/0.0095)² = 1.418 × 10⁶ min
tfield = 1.418 × 10⁶/1440 = 984.9 days

Answer

t = 984.9 days
17.Hydrostatic force

Answer: F = 176.6 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 = 2.5 + 3/2 = 4 m
A = H·b = 3·1.5 = 4.5 m²
gated = 2.5 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·4·4.5 = 176.6 kN

Answer

F = 176.6 kN
18.Hydrostatic force

Answer: F = 99.33 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 = 1.5 + 1.5/2 = 2.25 m
A = H·b = 1.5·3 = 4.5 m²
gated = 1.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.25·4.5 = 99.33 kN

Answer

F = 99.33 kN
19.Pipe friction & head loss

Answer: Δp = 42.67 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) = 0.02·(500/0.3)·1.6²/(2·9.81) = 4.349 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 = 1000·9.81·4.349 = 42667 Pa = 42.67 kPa

Answer

Δp = 42.67 kPa
20.Pipe friction & head loss

Answer: Δz = 5.072 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 = 0.15/0.07069 = 2.122 m/s
V²/(2g) = 0.2295 m

Loss coefficients

f·L/D = 0.018·300/0.3 = 18
ΣK = 0.5 + 2·0.3 + 2 + 1.0 = 4.1

Total head loss

hf = 18·0.2295 = 4.131 m
hm = 4.1·0.2295 = 0.941 m
Δz = hf + hm = 5.072 m

Answer

Δz = 5.072 m
21.Open-channel flow (Manning)

Answer: Q = 37.87 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 = 4·1.7 = 6.8 m²
P = b + 2y = 4 + 2·1.7 = 7.4 m
R = A/P = 0.9189 m

Velocity

V = (1/0.012)·0.91892/3·0.0051/2 = 5.57 m/s

Flow rate

Q = A·V = 6.8·5.57 = 37.87 m³/s

Answer

Q = 37.87 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.009812 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 = 0.25/4 = 0.0625 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·1.2/0.1575)² = 0.009812

Answer

S = 0.009812

That is a fall of 9.812 m per kilometre.

23.Pumps & pump power

Answer: Pel = 58.86 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 = 1000·9.81·0.06·72 = 42.38 kW

Shaft power

Pshaft = 42.38/0.8 = 52.97 kW

Electrical power

Pel = 52.97/0.9 = 58.86 kW

Answer

Pel = 58.86 kW
24.Pumps & pump power

Answer: H = 55.23 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 = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (30 + 8)·0.2905 = 11.04 m

Pressure head

p/(ρ·g) = 100000/(1000·9.81) = 10.19 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 34 + 10.19 + 11.04 = 55.23 m

Answer

H = 55.23 m
25.Time value of money

Answer: PV = 10898 €

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 = 0.04/12 = 0.003333
N = 12·8 = 96

Present value

PV = FV/(1 + i)N = 15 000/1.376 = €10 898.03

Answer

PV = €10 898.03
26.Time value of money

Answer: A = 442.6 €

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 = 0.024/12 = 0.002
N = 12·5 = 60

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 = 0.887
A = 25 000·0.002/(1 − 0.887) = €442.58

Answer

A = €442.58
27.NPV & IRR

Answer: NPV = −10046 €

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 + 0.06)1 = 14 000/1.06 = 13 207.55
CF2/(1 + 0.06)2 = 15 000/1.124 = 13 349.95
CF3/(1 + 0.06)3 = 10 000/1.191 = 8 396.19

Add them up

NPV = €−10 046.31

Answer

NPV = €−10 046.31

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

28.NPV & IRR

Answer: IRR = 30.16 %

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%) = 97.86
NPV(35%) = −2 790.73

Narrow down

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

IRR ≈ 30 + 5·97.86/(97.86 − (−2 790.73)) = 30.17%
exact: NPV(30.16%) = 0 → IRR = 30.16%

Answer

IRR = 30.16%
29.Normal distribution

Answer: P = 0.02275

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 = 105 s, σ = √(5² + 4²) = 6.403 s

Standardise

z = (117.8 − 105)/6.403 = 2

Upper tail

P = 1 − Φ(2) = 1 − 0.9772 = 0.02275

Answer

P = 0.02275
30.Normal distribution

Answer: x = 52.18 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) = 0.1 → z = −1.282

Back to x

x = 65 + −1.282·10 = 52.18 points

Answer

x = 52.18 points

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