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​ = 50 kNABRA​RB​ = ?1 m1 m3 m

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

L = 5 mP1 = 40 kN at 1 mP2 = 50 kN at 2 m
RB = kN
2.Beam support reactionsHard
w = 3 kN/mP = 25 kNABRA​RB​ = ?3.5 m1.5 m1 m

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

L = 6 mP = 25 kN at 3.5 mw = 3 kN/m from 0 to 5 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB25 kN6 m5 m2 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 = 2 mB is 5 m from Avertical load = 25 kN
FBC = kN
4.Truss: method of jointsHard
ABCDEFGH15 kN10 kN15 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: 15 kN ↓H: 10 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 = 6 kN/mABsection1.5 m6.5 m

Find the bending moment Mx at the section x = 1.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mw = 6 kN/m from 0 to 8 mx = 1.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 2 kN/mP = 60 kNAB6 m2 m

The simply supported beam carries a uniformly distributed load w over its whole span and a point load P. Find the maximum bending moment Mmax in the beam.

L = 8 mP = 60 kN at 6 mw = 2 kN/m from 0 to 8 m
Mmax = kN·m
7.Beam deflectionMedium
w = 10 kN/mδL = 3 m

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

w = 10 kN/mL = 3 mE = 11 GPa (timber)I = 120 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 5 kN/mAB6 m

A propped cantilever is fixed at A and simply supported (propped) at B. It carries a uniformly distributed load w over its whole length. EI is constant. Find the reaction RB at the prop.

L = 6 mw = 5 kN/m
RB = kN
9.Column bucklingMedium
PL = 5 md = 50 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)d = 50 mm
Pcr = kN
10.Column bucklingHard
PL = 5 md = 60 mmcross-section

A column of length L made of steel is pinned at both ends. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 5 mE = 200 GPa (steel)d = 60 mm
σcr = MPa
11.Centroid & second moment of areaMedium
160170t = 14xdimensions in mm

A channel section lies with its open side up: a base plate 160 mm wide with two upright legs, 170 mm high overall. Base and legs are all 14 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.

b = 160 mmh = 170 mmt = 14 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
100 mm150 mm97.5 mm40 × 40xIx​ = ?

A 100 mm × 150 mm plate has a rectangular cut-out 40 mm wide and 40 mm high, centred on the vertical centre line with its centre 97.5 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 100 mmh = 150 mmcut-out: 40 × 40 mmhole centre: y = 97.5 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 20.5 kN/m³14 mwater tableXz = 5 m

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

z = 5 mzw = 4 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 20.5 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 19 kN/m³4 mclayγsat​ = 17.5 kN/m³6 mwater tableXz = 7 m

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

z = 7 mzw = 2 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 19 kN/m³clay: γsat = 17.5 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 20 kPasandclayCc​ = 0.5, Cr​ = 0.02e0​ = 0.7σ′0​ = 120 kPaOCR = 1.57 mwater table

A 7 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.02 and e₀ = 0.7. At its mid-depth the effective vertical stress is 120 kPa and the overconsolidation ratio is OCR = 1.5. A new building adds 20 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7 mCc = 0.5Cr = 0.02e0 = 0.7σ′0 = 120 kPaOCR = 1.5Δσ = 20 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 4.5 m4.5 msandwater table

In a laboratory oedometer test, a clay specimen 25 mm thick, drained at the top and bottom, reaches 50% consolidation in 15 min. In the field the same clay forms a layer 4.5 m thick. It lies between two sand layers, so water drains out at the top and the bottom. How many days t does the field layer take to reach 50% consolidation?

hlab = 25 mmtlab = 15 minH = 4.5 mfield: double drainage
t = days
17.Hydrostatic forceMedium
gated = 2.5 mH = 2.5 m

A vertical rectangular gate 3 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 = 2.5 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2 mH = 3 m

A vertical rectangular gate 2 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 = 3 mb = 2 mρ = 880 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
Q = 25 L/sD = 150 mmL = 800 mf = 0.022

Water flows at 25 L/s through a pipe 800 m long with an inside diameter of 150 mm. Use the Darcy friction factor f = 0.022 and g = 9.81 m/s². Find the friction head loss hf.

Q = 25 L/sL = 800 mD = 150 mmf = 0.022g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10Δz = ?L = 300 m, D = 200 mm, f = 0.022× 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 = 0.02. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each), a valve (K = 10) 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 40 L/s?

Q = 40 L/sL = 300 mD = 200 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 10Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 3.5 my = 1.5 mn = 0.025, S = 0.003

A rectangular gravel channel is 3.5 m wide. Water flows uniformly 1.5 m deep. Manning n = 0.025 and the bed slope is S = 0.003. Find the flow rate Q in m³/s.

b = 3.5 my = 1.5 mn = 0.025S = 0.003
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 6 my = 1.6 m1 : 1n = 0.025, Q = 21 m³/s

A trapezoidal gravel channel with a bottom width of 6 m and side slopes of 1:1 (horizontal:vertical) must carry 21 m³/s in uniform flow at a depth of 1.6 m. Manning n = 0.025. Find the required bed slope S (in m/m).

Q = 21 m³/sb = 6 my = 1.6 mz = 1n = 0.025
S = m/m
23.Pumps & pump powerMedium
PQ = 20 L/sH = 78 m

A pump with an efficiency of 85% delivers 20 L/s of water (ρ = 1000 kg/m³) against a head of 78 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 20 L/sH = 78 mη = 85%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 60 L/sΔz = 7 mL = 300 m, D = 200 mm, f = 0.022, ΣK = 4

A pump moves 60 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 300 m long with an inside diameter of 200 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 pump efficiency is 75%. Find the shaft power Pshaft in kW.

Q = 60 L/sΔz = 7 mL = 300 mD = 200 mmf = 0.022ΣK = 4η = 75%
Pshaft = kW
25.Time value of moneyMedium
years0123…10€8 000FV = ?

You invest €8 000 at a nominal rate of 2% per year, compounded monthly. Find the value FV of the investment after 10 years.

PV = €8 0002% / 12n = 10
FV = €
26.Time value of moneyHard
months0123…N = ?€15 000€350€350€350€3504.2% / 12

You borrow €15 000 at 4.2% per year, compounded monthly, and repay €350 at the end of every month. How many months does it take until the loan is repaid (the last payment may be smaller)? Give the number of payments N.

P = €15 000A = €3504.2% / 12
N = payments
27.NPV & IRRMedium
years012345−50 00010 00010 00010 00010 00015 000

A machine costs €50 000 today. It generates €10 000 at the end of each year for 5 years and can then be sold for €5 000. The cost of capital is 10%. Find the net present value NPV.

C0 = €50 000CF = €10 000S = €5 000n = 5r = 10%
NPV = €
28.NPV & IRRHard
years01234−40 00012 50017 00022 00012 500

A project costs €40 000 and returns €12 500, €17 000, €22 000, €12 500 at the end of years 1 to 4. Cash flows can be reinvested at the cost of capital of 8%. Find the modified internal rate of return MIRR in percent.

r = 8%CF0 = −40 000CF1 = 12 500CF2 = 17 000CF3 = 22 000CF4 = 12 500
MIRR = %
29.Normal distributionMedium
150 kg148.2 kgT = X₁ + … + X₆?

The masses of bags of cement are independent and normal with mean 25 kg and standard deviation 0.5 kg. Find the probability P that the total mass of 6 of them is below 148.2 kg. Round z to two decimals.

μ = 25 kgσ = 0.5 kgn = 6< 148.2 kg
P =
30.Normal distributionHard
μ = 178x = ?25%

The heights of adult men are normally distributed with mean 178 cm and standard deviation 7 cm. Find the value x below which 25% of them lie (the 25th percentile).

μ = 178σ = 7P = 25%
x = cm

3Solutions

1.Beam support reactions

Answer: RB = 28 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​ = 50 kNABRA​RB​1 m1 m3 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·5 = 40·1 + 50·2
RB = 140/5 = 28 kN
ΣFy = 0: RA = 90 − 28 = 62 kN

Answer

RB = 28 kN
2.Beam support reactions

Answer: RB = 20.83 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 = 3 kN/mP = 25 kNABRA​RB​3.5 m1.5 m1 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 3·5 = 15 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·6 = 25·3.5 + 3·5·2.5
RB = 125/6 = 20.83 kN
ΣFy = 0: RA = 40 − 20.83 = 19.17 kN

Answer

RB = 20.83 kN
3.Truss: method of joints

Answer: FBC = −23.29 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 25·5 → Cy = 20.83 kN
ΣFy = 0: Ay = 25 − 20.83 = 4.167 kN

Joint C

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

sin γ = 2/2.236 = 0.8944, cos γ = 1/2.236 = 0.4472
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −20.83/0.8944 = −23.29 kN

Answer

FBC = −23.29 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: 5 kN (C), BC: 5 kN (T), CD: 5 kN (T), DE: 15 kN (T), FG: 10 kN (C), GH: 30 kN (C), AF: 14.14 kN (C), HE: 21.21 kN (C), BF: 10 kN (T), CG: 0, DH: 5 kN (T), BG: 14.14 kN (C), DG: 14.14 kN (T)

Answer

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

Answer: Mx = 29.25 kN·m

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

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 6·8 = 48 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 6·8·4
RB = 192/8 = 24 kN
ΣFy = 0: RA = 48 − 24 = 24 kN
w = 6 kN/mABRA​ = 24RB​ = 24section1.5 m6.5 m

Cut at x = 1.5 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 = 24·1.5 − 6·1.5·0.75 = 29.25 kN·m

Answer

Mx = 29.25 kN·m
6.Shear force & bending moment

Answer: Mmax = 102 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.

UDL resultant: W = w·ℓ = 2·8 = 16 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 60·6 + 2·8·4
RB = 424/8 = 53 kN
ΣFy = 0: RA = 76 − 53 = 23 kN

Where is V = 0?

V(6⁻) = RA − w·6 = 11 kN
V(6⁺) = 11 − 60 = −49 kN
The shear changes sign at the load, so the maximum is under the load.

Maximum moment

Mmax = RA·6 − w·6²/2 = 23·6 − 2·6²/2 = 102 kN·m

Answer

Mmax = 102 kN·m

It occurs at x = 6 m from A.

7.Beam deflection

Answer: δmax = 7.99 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 = 10 N/mm, L = 3000 mm
EI = 1.32 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·10·3000⁴/(384·1.32 × 10¹²) = 7.99 mm

Answer

δmax = 7.99 mm
8.Beam deflection

Answer: RB = 11.25 kN

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 = wL⁴/(8EI)

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) = wL⁴/(8EI) → RB = 3wL/8 = 3·5·6/8 = 11.25 kN

Answer

RB = 11.25 kN
9.Column buckling

Answer: Pcr = 33.91 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·50⁴/64 = 306796 mm⁴

Effective length

KL = 0.5·5000 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·306796/2500² = 33913 N = 33.91 kN

Answer

Pcr = 33.91 kN
10.Column buckling

Answer: σcr = 17.77 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·60⁴/64 = 636173 mm⁴

Radius of gyration and slenderness

A = 2827 mm²
r = √(I/A) = √(636173/2827) = 15 mm
KL = 1·5000 = 5000 mm
KL/r = 5000/15 = 333.3

Critical stress

σcr = π²E/(KL/r)² = π²·200000/333.3² = 17.77 MPa

Answer

σcr = 17.77 MPa
11.Centroid & second moment of area

Answer: Ix = 19.59 × 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 rectangles

Take the base at full width and the two legs above it (height h − t), so nothing is counted twice.

base: A1 = 160·14 = 2240 mm², y1 = 7 mm
two legs: A2 = 2·14·156 = 4368 mm², y2 = 14 + 156/2 = 92 mm

Centroid

ȳ = (2240·7 + 4368·92)/6608 = 63.19 mm

Parallel-axis theorem

base: 160·14³/12 + 2240·(7 − 63.19)² = 7.108 × 10⁶ mm⁴
two legs: 2·14·156³/12 + 4368·(92 − 63.19)² = 1.248 × 10⁷ mm⁴
Ix = 7.108 × 10⁶ + 1.248 × 10⁷
Ix = 1.959 × 10⁷ mm⁴ = 19.59 × 10⁶ mm⁴

Answer

Ix = 19.59 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 27 × 10⁶ mm⁴

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

Centroid

ȳ = (15000·75 − 1600·97.5)/(15000 − 1600) = 72.31 mm

Full plate about ȳ

100·150³/12 + 15000·2.687² = 28.23 × 10⁶ mm⁴

Hole about ȳ

40·40³/12 + 1600·25.19² = 1.228 × 10⁶ mm⁴

Subtract

Ix = 27 × 10⁶ mm⁴

Answer

Ix = 27 × 10⁶ mm⁴
13.Effective stress in soil

Answer: u = 9.81 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) = 9.81·1 = 9.81 kPa

Answer

u = 9.81 kPa
14.Effective stress in soil

Answer: u = 49.05 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) = 9.81·5 = 49.05 kPa

Answer

u = 49.05 kPa
15.Consolidation settlement

Answer: S = 5.513 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 = 1.5·120 = 180 kPa

Compare with the preconsolidation pressure

σ′f = 120 + 20 = 140 kPa ≤ 180 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.02·7/(1 + 0.7)·log₁₀(140/120) = 5.513 mm

Answer

S = 5.513 mm
16.Consolidation settlement

Answer: t = 337.5 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 = 25/2 = 12.5 mm = 0.0125 m
Hdr,field = 4.5/2 = 2.25 m

Scale the time

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

tfield = 15·(2.25/0.0125)² = 486000 min
tfield = 486000/1440 = 337.5 days

Answer

t = 337.5 days
17.Hydrostatic force

Answer: F = 275.9 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 + 2.5/2 = 3.75 m
A = H·b = 2.5·3 = 7.5 m²
gated = 2.5 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.75·7.5 = 275.9 kN

Answer

F = 275.9 kN
18.Hydrostatic force

Answer: ycp = 3.714 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 + 3/2 = 3.5 m
A = H·b = 3·2 = 6 m²
gated = 2 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·3.5·6 = 181.3 kN

Centre of pressure

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

Ic = b·H³/12 = 2·3³/12 = 4.5 m⁴
ycp = yc + Ic/(yc·A) = 3.5 + 4.5/(3.5·6) = 3.714 m

Answer

ycp = 3.714 m
19.Pipe friction & head loss

Answer: hf = 11.97 m

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

Mean velocity

A = π·0.15²/4 = 0.01767 m²
V = Q/A = 0.025/0.01767 = 1.415 m/s

Velocity head

V²/(2g) = 1.415²/(2·9.81) = 0.102 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.022·(800/0.15)·1.415²/(2·9.81) = 11.97 m

Answer

hf = 11.97 m
20.Pipe friction & head loss

Answer: Δz = 3.479 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 = 0.02·300/0.2 = 30
ΣK = 0.5 + 2·0.3 + 10 + 1.0 = 12.1

Total head loss

hf = 30·0.08263 = 2.479 m
hm = 12.1·0.08263 = 0.9998 m
Δz = hf + hm = 3.479 m

Answer

Δz = 3.479 m
21.Open-channel flow (Manning)

Answer: Q = 9.976 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 = 3.5·1.5 = 5.25 m²
P = b + 2y = 3.5 + 2·1.5 = 6.5 m
R = A/P = 0.8077 m

Velocity

V = (1/0.025)·0.80772/3·0.0031/2 = 1.9 m/s

Flow rate

Q = A·V = 5.25·1.9 = 9.976 m³/s

Answer

Q = 9.976 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.001538 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 = (6 + 1·1.6)·1.6 = 12.16 m²
P = b + 2y·√(1 + z²) = 6 + 2·1.6·√(1 + 1²) = 10.53 m
R = A/P = 1.155 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.025·21/(12.16·1.101) = 0.03921
S = 0.03921² = 0.001538

Answer

S = 0.001538

That is a fall of 1.538 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 18 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 = 1000·9.81·0.02·78 = 15.3 kW

Shaft power

Pshaft = Ph/η = 15.3/0.85 = 18 kW

Answer

Pshaft = 18 kW
24.Pumps & pump power

Answer: Pshaft = 10.89 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 = 0.06/0.03142 = 1.91 m/s
V²/(2g) = 0.1859 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (33 + 4)·0.1859 = 6.879 m

Pump head

H = Δz + hL = 7 + 6.879 = 13.88 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.06·13.88/0.75 = 10.89 kW

Answer

Pshaft = 10.89 kW
25.Time value of money

Answer: FV = 9770 €

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 = r/m = 0.02/12 = 0.001667
N = m·n = 12·10 = 120

Future value

FV = 8 000·(1 + 0.001667)120 = 8 000·1.221 = €9 769.60

Answer

FV = €9 769.60
26.Time value of money

Answer: N = 47 payments

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.

Rearrange the annuity formula

i = 0.0035
(1 + i)−N = 1 − 15 000·0.0035/350 = 0.85

Solve with logarithms

N = −ln(0.85)/ln(1.004) = 46.52

Round up to whole payments

46 full payments leave a small balance, which the last, smaller payment clears.

N = 47

Answer

N = 47 payments
27.NPV & IRR

Answer: NPV = −8988 €

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

Present value of the yearly cash flows

10 000·3.791 = 37 907.87

Present value of the salvage value

5 000/1.611 = 3 104.61

NPV

NPV = −50 000 + 37 907.87 + 3 104.61 = −€8 987.53

Answer

NPV = −€8 987.53
28.NPV & IRR

Answer: MIRR = 15.76 %

Modified IRR: compound every inflow forward to the end of the project at the reinvestment rate (usually the cost of capital) to get the terminal value TV. MIRR is the rate that turns the initial investment into TV: MIRR = (TV/C₀)^(1/n) − 1.

Terminal value of the inflows

12 500·1.083 = 15 746.40
17 000·1.082 = 19 828.80
22 000·1.081 = 23 760.00
12 500·1.080 = 12 500.00
TV = 71 835.20

MIRR

MIRR = (71 835.20/40 000)1/4 − 1 = 15.76%

Answer

MIRR = 15.76%
29.Normal distribution

Answer: P = 0.07078

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 total

μT = 150 kg, σT = 0.5·√6 = 1.225 kg

Standardise

z = (148.2 − 150)/1.225 = −1.47

Probability

P = Φ(−1.47) = 0.07078

Answer

P = 0.07078
30.Normal distribution

Answer: x = 173.3 cm

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 = 178 + −0.6745·7 = 173.28 cm

Answer

x = 173.28 cm

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