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​ = 80 kNP2​ = 45 kNABCRB​ = ?1 m2 m1 m

The beam has a pin at A and a roller at B, 3 m from A, and overhangs B to the free end C. Find the vertical reaction RB, taking upward as positive.

AB = 3 mAC = 4 mP1 = 80 kN at 1 mP2 = 45 kN at 4 m
RB = kN
2.Beam support reactionsHard
w = 5 kN/mP = 60 kNABRA​RB​ = ?1 m2 m7 m

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

L = 10 mP = 60 kN at 3 mw = 5 kN/m from 0 to 1 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB10 kN6 m5 m4 m

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

span = 6 mheight = 4 mB is 5 m from Avertical load = 10 kN
FAB = kN
4.Truss: method of jointsHard
ABCDEFGH35 kN25 kN20 kN25 kN4 × 4 m4 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 ↓F: 25 kN ↓F: 20 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 FC
  13. 13member HC
5.Shear force & bending momentMedium
w = 6 kN/mABsection6 m2 m

Find the shear force Vx at the section x = 6 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 = 6 m
Vx = kN
6.Shear force & bending momentHard
w = 8 kN/mP = 20 kNABsection4 m4 m2 m

Find the bending moment Mx at the section x = 4 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mP = 20 kN at 8 mw = 8 kN/m from 0 to 10 mx = 4 m
Mx = kN·m
7.Beam deflectionMedium
w = 6 kN/mδL = 2 m

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

w = 6 kN/mL = 2 mE = 11 GPa (timber)I = 36 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
P = 80 kNAB2 m2 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 = 4 mP = 80 kN at 2 m
MA = kN·m
9.Column bucklingMedium
PL = 2 m25 × 60 mmcross-section

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

L = 2 mE = 200 GPa (steel)b × h = 25 × 60 mm
Pcr = kN
10.Column bucklingHard
P = 70 kNL = 4 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and pinned at the top. It must carry 70 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 70 kNn = 3L = 4 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
200 mm150 mm105 mmØ60xIx​ = ?

A 200 mm × 150 mm plate has a circular hole of diameter 60 mm on its vertical centre line, with its centre 105 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 200 mmh = 150 mmd = 60 mmhole centre: y = 105 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
100 mm240 mm72 mm30 × 20xIx​ = ?

A 100 mm × 240 mm plate has a rectangular cut-out 30 mm wide and 20 mm high, centred on the vertical centre line with its centre 72 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 100 mmh = 240 mmcut-out: 30 × 20 mmhole centre: y = 72 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 18.5 kN/m³12 mwater tableXz = 6 m

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

z = 6 mzw = 4 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 18.5 kN/m³
σ = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 19 kN/m³4 mclayγsat​ = 17.5 kN/m³4 mwater tableXz = 6 m

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

z = 6 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19 kN/m³clay: γsat = 17.5 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 170 kPasandclayCc​ = 0.35, Cr​ = 0.02e0​ = 0.9σ′0​ = 105 kPaσ′p​ = 165 kPa6 mwater table

A 6 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.02 and e₀ = 0.9. At its mid-depth the effective vertical stress is 105 kPa and the preconsolidation pressure is 165 kPa. A new building adds 170 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 6 mCc = 0.35Cr = 0.02e0 = 0.9σ′0 = 105 kPaσ′p = 165 kPaΔσ = 170 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 4.5 mcv​ = 1 m²/year4.5 msandwater table

A clay layer 4.5 m thick has a coefficient of consolidation cv = 1 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 90% average consolidation the time factor is Tv = 0.848. How many years t does the layer take to reach 90% consolidation?

H = 4.5 mcv = 1 m²/yearU = 90%Tv = 0.848double drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 2 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 2 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2 mH = 1.5 m

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

d = 2 mH = 1.5 mb = 1.5 mρ = 880 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1.4 m/sD = 150 mmL = 1000 mf = 0.015

Water (ρ = 1000 kg/m³) flows at 1.4 m/s through a horizontal pipe, 1000 m long, with an inside diameter of 150 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 = 1.4 m/sL = 1000 mD = 150 mmf = 0.015ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 2free outletH = ?L = 200 m, D = 150 mm, f = 0.023× bend (K = 0.3)

A pipe 200 m long with an inside diameter of 150 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 = 2). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 20 L/s?

Q = 20 L/sL = 200 mD = 150 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 2
H = m
21.Open-channel flow (Manning)Medium
b = 3 my = 2.1 mn = 0.014, S = 0.0015

A rectangular unfinished concrete channel is 3 m wide. Water flows uniformly 2.1 m deep. Manning n = 0.014 and the bed slope is S = 0.0015. Find the flow rate Q in m³/s.

b = 3 my = 2.1 mn = 0.014S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 5.5 my = 1.6 m1 : 1n = 0.025, Q = 16 m³/s

A trapezoidal gravel channel with a bottom width of 5.5 m and side slopes of 1:1 (horizontal:vertical) must carry 16 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 = 16 m³/sb = 5.5 my = 1.6 mz = 1n = 0.025
S = m/m
23.Pumps & pump powerMedium
PQ = 10 L/sH = 20 m

A pump with an efficiency of 80% delivers 10 L/s of water (ρ = 1000 kg/m³) against a head of 20 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 10 L/sH = 20 mη = 80%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 75 L/sΔz = 16 mL = 400 m, D = 200 mm, f = 0.02, 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 16 m higher. The pipe is 400 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 75 L/sΔz = 16 mL = 400 mD = 200 mmf = 0.02ΣK = 8
H = m
25.Time value of moneyMedium
years0123…8€20 000FV = ?

You invest €20 000 at a nominal rate of 3.6% per year, compounded monthly. Find the value FV of the investment after 8 years.

PV = €20 0003.6% / 12n = 8
FV = €
26.Time value of moneyHard
months01…228…360€200 000AB = ?A5.4% / 12

A mortgage of €200 000 is repaid with equal monthly payments over 30 years at 5.4% per year, compounded monthly. How much is still owed just after the payment at the end of year 19? Find the outstanding balance B.

P = €200 0005.4% / 12N = 360k = 228
B = €
27.NPV & IRRMedium
years01234−45 00015 0009 00018 00013 000

An investment of €45 000 gives these cash flows at the end of years 1 to 4: €15 000, €9 000, €18 000, €13 000. The cost of capital is 10%. Find the net present value NPV.

r = 10%CF0 = −45 000CF1 = 15 000CF2 = 9 000CF3 = 18 000CF4 = 13 000
NPV = €
28.NPV & IRRHard
years0123−40 00027 00016 00018 500

A project costs €40 000 and returns €27 000, €16 000, €18 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 27 000CF2 = 16 000CF3 = 18 500
IRR = %
29.Normal distributionMedium
5785P = ?

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. What fraction lies between 57 and 85 points? Give P as a decimal.

μ = 65σ = 10x1 = 57x2 = 85
P =
30.Normal distributionHard
μ = 250x = ?20%

The bag weights are normally distributed with mean 250 g and standard deviation 5 g. Find the value x below which 20% of them lie (the 20th percentile).

μ = 250σ = 5P = 20%
x = g

3Solutions

1.Beam support reactions

Answer: RB = 86.67 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Replace each distributed load by its resultant (its area) acting at the centroid of the load diagram, and take moments about a support to remove that support’s reaction from the equation.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·3 = 80·1 + 45·4
RB = 260/3 = 86.67 kN

Vertical equilibrium

RA = 80 + 45 − 86.67 = 38.33 kN

Answer

RB = 86.67 kN
2.Beam support reactions

Answer: RB = 18.25 kN

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

w = 5 kN/mP = 60 kNABRA​RB​1 m2 m7 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 = 5·1 = 5 kN, acting at x̄ = 0.5 m
ΣMA = 0: RB·10 = 60·3 + 5·1·0.5
RB = 182.5/10 = 18.25 kN
ΣFy = 0: RA = 65 − 18.25 = 46.75 kN

Answer

RB = 18.25 kN
3.Truss: method of joints

Answer: FAB = −2.668 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.

ABBCACACB10 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 10·5 → Cy = 8.333 kN
ΣFy = 0: Ay = 10 − 8.333 = 1.667 kN

Joint A

Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.

sin α = 4/6.403 = 0.6247
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −1.667/0.6247 = −2.668 kN

Answer

FAB = −2.668 kN (compression)
4.Truss: method of joints

Answer: member BF

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 B

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

ΣF⊥ = 0 → FBF = 0

Check with the method of joints

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

AB: 55 kN (T), BC: 55 kN (T), CD: 50 kN (T), DE: 50 kN (T), FG: 65 kN (C), GH: 65 kN (C), AF: 49.5 kN (C), HE: 70.71 kN (C), BF: 0, CG: 25 kN (C), DH: 35 kN (T), FC: 14.14 kN (T), HC: 21.21 kN (T)

Answer

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

Answer: Vx = −12 kN

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​ = 24section6 m2 m

Cut at x = 6 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.

V = RA − (all downward loads left of the cut)
Vx = 24 − 6·6 = −12 kN

Answer

Vx = −12 kN
6.Shear force & bending moment

Answer: Mx = 112 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 = 8·10 = 80 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 20·8 + 8·10·5
RB = 560/10 = 56 kN
ΣFy = 0: RA = 100 − 56 = 44 kN
w = 8 kN/mP = 20 kNABRA​ = 44RB​ = 56section4 m4 m2 m

Cut at x = 4 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 = 44·4 − 8·4·2 = 112 kN·m

Answer

Mx = 112 kN·m
7.Beam deflection

Answer: δmax = 3.157 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 = 6 N/mm, L = 2000 mm
EI = 3.96 × 10¹¹ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·6·2000⁴/(384·3.96 × 10¹¹) = 3.157 mm

Answer

δmax = 3.157 mm
8.Beam deflection

Answer: MA = 60 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 = 5·80/16 = 25 kN

Moment at the fixed end

Moments about A of the loads and the prop force.

MA = P·L/2 − RB·L = 160 − 100 = 60 kN·m

Answer

MA = 60 kN·m
9.Column buckling

Answer: Pcr = 154.2 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 = 60·25³/12 = 78125 mm⁴

Effective length

KL = 0.5·2000 = 1000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·78125/1000² = 154213 N = 154.2 kN

Answer

Pcr = 154.2 kN
10.Column buckling

Answer: d = 64.2 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 = 3·70000 = 210000 N
KL = 0.7·4000 = 2800 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·210000·2800²/(π³·200000))^(1/4) = 64.2 mm

Answer

d = 64.2 mm

Check: the slenderness KL/r is 174.4, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 52.8 × 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 = (30000·75 − 2827·105)/(30000 − 2827) = 71.88 mm

Full plate about ȳ

200·150³/12 + 30000·3.122² = 56.54 × 10⁶ mm⁴

Hole about ȳ

π·60⁴/64 + 2827·33.12² = 3.738 × 10⁶ mm⁴

Subtract

Ix = 52.8 × 10⁶ mm⁴

Answer

Ix = 52.8 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 113.8 × 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 = (24000·120 − 600·72)/(24000 − 600) = 121.2 mm

Full plate about ȳ

100·240³/12 + 24000·−1.231² = 115.2 × 10⁶ mm⁴

Hole about ȳ

30·20³/12 + 600·−49.23² = 1.474 × 10⁶ mm⁴

Subtract

Ix = 113.8 × 10⁶ mm⁴

Answer

Ix = 113.8 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ = 101 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) = 16·4 + 18.5·2 = 101 kPa

Answer

σ = 101 kPa
14.Effective stress in soil

Answer: u = 29.43 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) = 9.81·3 = 29.43 kPa

Answer

u = 29.43 kPa
15.Consolidation settlement

Answer: S = 257.6 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 = 105 + 170 = 275 kPa > 165 kPa

Settlement

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

S = 0.02·6/(1 + 0.9)·log₁₀(165/105) + 0.35·6/(1 + 0.9)·log₁₀(275/165)
S = 12.4 + 245.2 = 257.6 mm

Answer

S = 257.6 mm
16.Consolidation settlement

Answer: t = 4.293 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/2 = 4.5/2 = 2.25 m

Time

t = Tv·Hdr²/cv = 0.848·2.25²/1 = 4.293 years

Answer

t = 4.293 years
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 + 2/2 = 3 m
A = H·b = 2·3 = 6 m²
gated = 2 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3·6 = 176.6 kN

Answer

F = 176.6 kN
18.Hydrostatic force

Answer: F = 53.42 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 + 1.5/2 = 2.75 m
A = H·b = 1.5·1.5 = 2.25 m²
gated = 2 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·2.75·2.25 = 53.42 kN

Answer

F = 53.42 kN
19.Pipe friction & head loss

Answer: Δp = 98 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·(1000/0.15)·1.4²/(2·9.81) = 9.99 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 = 1000·9.81·9.99 = 98000 Pa = 98 kPa

Answer

Δp = 98 kPa
20.Pipe friction & head loss

Answer: H = 2.028 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 = 0.02/0.01767 = 1.132 m/s
V²/(2g) = 0.06529 m

Loss coefficients

f·L/D = 0.02·200/0.15 = 26.67
ΣK = 0.5 + 3·0.3 + 2 = 3.4

Energy equation

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

H = (1 + 26.67 + 3.4)·0.06529 = 2.028 m

Answer

H = 2.028 m
21.Open-channel flow (Manning)

Answer: Q = 15.94 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 = 3·2.1 = 6.3 m²
P = b + 2y = 3 + 2·2.1 = 7.2 m
R = A/P = 0.875 m

Velocity

V = (1/0.014)·0.8752/3·0.00151/2 = 2.531 m/s

Flow rate

Q = A·V = 6.3·2.531 = 15.94 m³/s

Answer

Q = 15.94 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.00105 m/m

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

Geometry

A = (b + z·y)·y = (5.5 + 1·1.6)·1.6 = 11.36 m²
P = b + 2y·√(1 + z²) = 5.5 + 2·1.6·√(1 + 1²) = 10.03 m
R = A/P = 1.133 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.025·16/(11.36·1.087) = 0.0324
S = 0.0324² = 0.00105

Answer

S = 0.00105

That is a fall of 1.05 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 2.453 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 = 1000·9.81·0.01·20 = 1.962 kW

Shaft power

Pshaft = Ph/η = 1.962/0.8 = 2.453 kW

Answer

Pshaft = 2.453 kW
24.Pumps & pump power

Answer: H = 29.94 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) = (40 + 8)·0.2905 = 13.94 m

Pump head

Both surfaces are open and practically at rest, so pressure and velocity terms drop out.

H = Δz + hL = 16 + 13.94 = 29.94 m

Answer

H = 29.94 m
25.Time value of money

Answer: FV = 26664 €

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 = 0.036000000000000004/12 = 0.003
N = m·n = 12·8 = 96

Future value

FV = 20 000·(1 + 0.003)96 = 20 000·1.333 = €26 663.65

Answer

FV = €26 663.65
26.Time value of money

Answer: B = 111595 €

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 payment

i = 0.0045, N = 360
A = 200 000·0.0045/(1 − (1 + 0.0045)−360) = €1 123.06

Present value of the remaining payments

Whatever is still owed must be exactly paid off by the remaining payments.

N − k = 360 − 228 = 132
B = 1123·(1 − (1 + 0.0045)−132)/0.0045 = €111 594.74

Answer

B = €111 594.74
27.NPV & IRR

Answer: NPV = −1523 €

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 + 0.1)1 = 15 000/1.1 = 13 636.36
CF2/(1 + 0.1)2 = 9 000/1.21 = 7 438.02
CF3/(1 + 0.1)3 = 18 000/1.331 = 13 523.67
CF4/(1 + 0.1)4 = 13 000/1.464 = 8 879.17

Add them up

NPV = €−1 522.78

Answer

NPV = €−1 522.78

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

28.NPV & IRR

Answer: IRR = 27.4 %

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(25%) = 1 312.00
NPV(30%) = −1 342.74

Narrow down

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

IRR ≈ 25 + 5·1 312.00/(1 312.00 − (−1 342.74)) = 27.47%
exact: NPV(27.4%) = 0 → IRR = 27.4%

Answer

IRR = 27.4%
29.Normal distribution

Answer: P = 0.7654

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 = (57 − 65)/10 = −0.8
z₂ = (85 − 65)/10 = 2

Area between

P = Φ(2) − Φ(−0.8) = 0.9772 − 0.2119 = 0.7654

Answer

P = 0.7654
30.Normal distribution

Answer: x = 245.8 g

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) = 0.2 → z = −0.8416

Back to x

x = 250 + −0.8416·5 = 245.79 g

Answer

x = 245.79 g

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