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
w0​ = 10 kN/mABRA​ = ?6 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that falls from 10 kN/m at A to zero at B. Find the vertical support reaction RA.

L = 6 mw0 = 10 kN/m
RA = kN
2.Beam support reactionsHard
w0​ = 12 kN/mP = 60 kNABMA​ = ?4 m4 m

The cantilever beam is fixed to the wall at A. It carries a linearly varying load that is 12 kN/m at the wall and falls to zero at the free end B, plus a point load P at 4 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 8 mw0 = 12 kN/mP = 60 kN at 4 m
MA = kN·m
3.Truss: method of jointsMedium
ABBCACACB10 kN6 m1 m3 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 = 3 mB is 1 m from Avertical load = 10 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB55 kN30 kN8 m1 m4 m

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

span = 8 mheight = 4 mB is 1 m from Avertical load = 55 kNhorizontal load = 30 kN →
FAB = kN
5.Shear force & bending momentMedium
60 kN25 kNABCDEFG2 m2 m2 m2 m2 m2 m

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

60 kN @ 8 m25 kN @ 6 m
  1. 1A (x = 0 m)
  2. 2B (x = 2 m)
  3. 3C (x = 4 m)
  4. 4D (x = 6 m)
  5. 5E (x = 8 m)
  6. 6F (x = 10 m)
  7. 7G (x = 12 m)
6.Shear force & bending momentHard
w = 5 kN/mP = 45 kNABsection5 m1 m2 m

Find the bending moment Mx at the section x = 5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 45 kN at 6 mw = 5 kN/m from 0 to 8 mx = 5 m
Mx = kN·m
7.Beam deflectionMedium
w = 20 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 = 20 kN/mL = 2 mE = 11 GPa (timber)I = 8.5 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
P = 16 kNP = 16 kNABδ1.667 m1.666 m1.667 m

A simply supported beam carries two equal point loads P at its third points (L/3 from each support). Using superposition, find the midspan deflection δmax.

P = 16 kNL = 5 mE = 11 GPa (timber)I = 160 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 2 md = 25 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 = 2 mE = 70 GPa (aluminium)d = 25 mm
Pcr = kN
10.Column bucklingHard
PL = 6 md = 80 mmcross-section

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

L = 6 mE = 200 GPa (steel)d = 80 mm
σcr = MPa
11.Centroid & second moment of areaMedium
100 mm150 mm105 mmØ60xIx​ = ?

A 100 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 = 100 mmh = 150 mmd = 60 mmhole centre: y = 105 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
280101608xM = 10 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 10 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 280 mmtf = 10 mmtw = 8 mmhw = 160 mmM = 10 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 20.5 kN/m³7 mwater tableXz = 6 m

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

z = 6 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​ = 16 kN/m³γsat​ = 19.5 kN/m³6 mclayγsat​ = 18.5 kN/m³6 mwater tableXz = 9 m

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

z = 9 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19.5 kN/m³clay: γsat = 18.5 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 160 kPasandclayCc​ = 0.25, Cr​ = 0.03e0​ = 0.9σ′0​ = 105 kPaσ′p​ = 165 kPa6 mwater table

A 6 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.03 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 160 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 6 mCc = 0.25Cr = 0.03e0 = 0.9σ′0 = 105 kPaσ′p = 165 kPaΔσ = 160 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 6.5 m6.5 msandwater table

In a laboratory oedometer test, a clay specimen 20 mm thick, drained at the top and bottom, reaches 50% consolidation in 12 min. In the field the same clay forms a layer 6.5 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 = 20 mmtlab = 12 minH = 6.5 mfield: double drainage
t = days
17.Hydrostatic forceMedium
gated = 1 mH = 2.5 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of water, with its top edge 1 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1 mH = 2.5 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2.5 mH = 1.5 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 depth ycp of the centre of pressure below the surface.

d = 2.5 mH = 1.5 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 1.6 m/sD = 250 mmL = 1000 mf = 0.02

Water flows at a mean velocity of 1.6 m/s through a pipe 1000 m long with an inside diameter of 250 mm. Use the Darcy friction factor f = 0.02 and g = 9.81 m/s². Find the friction head loss hf.

V = 1.6 m/sL = 1000 mD = 250 mmf = 0.02g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5free outletH = ?L = 200 m, D = 250 mm, f = 0.0223× bend (K = 0.3)

A pipe 200 m long with an inside diameter of 250 mm (Darcy friction factor f = 0.022) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each) and a valve (K = 5). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 80 L/s?

Q = 80 L/sL = 200 mD = 250 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5
H = m
21.Open-channel flow (Manning)Medium
b = 4.5 my = 0.6 mn = 0.015, S = 0.004

A rectangular brickwork channel is 4.5 m wide. Water flows uniformly 0.6 m deep. Manning n = 0.015 and the bed slope is S = 0.004. Find the flow rate Q in m³/s.

b = 4.5 my = 0.6 mn = 0.015S = 0.004
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2.5 my = 0.6 m2 : 1n = 0.025, Q = 3.6 m³/s

A trapezoidal gravel channel with a bottom width of 2.5 m and side slopes of 2:1 (horizontal:vertical) must carry 3.6 m³/s in uniform flow at a depth of 0.6 m. Manning n = 0.025. Find the required bed slope S (in m/m).

Q = 3.6 m³/sb = 2.5 my = 0.6 mz = 2n = 0.025
S = m/m
23.Pumps & pump powerMedium
PQ = 30 L/sH = 58 m

A pump delivers 30 L/s of water (ρ = 1000 kg/m³) against a head of 58 m. The pump efficiency is 82% and the electric motor driving it has an efficiency of 94%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 30 L/sH = 58 mηpump = 82%ηmotor = 94%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 20 L/sΔz = 14 mL = 150 m, D = 100 mm, f = 0.022, ΣK = 6

A pump moves 20 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 14 m higher. The pipe is 150 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 65%. Find the shaft power Pshaft in kW.

Q = 20 L/sΔz = 14 mL = 150 mD = 100 mmf = 0.022ΣK = 6η = 65%
Pshaft = kW
25.Time value of moneyMedium
years0123€5 000FV = ?

You invest €5 000 at a nominal rate of 4.8% per year, compounded monthly. Find the value FV of the investment after 3 years.

PV = €5 0004.8% / 12n = 3
FV = €
26.Time value of moneyHard
months0123…72€30 000AAAA5.4% / 12, I = ?

A loan of €30 000 is repaid with equal monthly payments over 6 years at 5.4% per year, compounded monthly. How much interest I is paid in total over the life of the loan?

P = €30 0005.4% / 12N = 72
I = €
27.NPV & IRRMedium
years0123−60 00016 00018 00030 000

An investment of €60 000 gives these cash flows at the end of years 1 to 3: €16 000, €18 000, €30 000. The cost of capital is 8%. Find the net present value NPV.

r = 8%CF0 = −60 000CF1 = 16 000CF2 = 18 000CF3 = 30 000
NPV = €
28.NPV & IRRHard
years0123−40 00015 00029 50021 500

A project costs €40 000 and returns €15 000, €29 500, €21 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 15 000CF2 = 29 500CF3 = 21 500
IRR = %
29.Normal distributionMedium
96.25107.5P = ?

The IQ scores are normally distributed with mean 100 points and standard deviation 15 points. What fraction lies between 96.25 and 107.5 points? Give P as a decimal.

μ = 100σ = 15x1 = 96.25x2 = 107.5
P =
30.Normal distributionHard
380420460500540580620hbottom 5%

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. Drag the cut-off so the shaded bottom 5% is to the left of it. Find the cut-off x.

μ = 500 hσ = 40 h5%
x = h

3Solutions

1.Beam support reactions

Answer: RA = 20 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.

Resultant of the triangular load

W = ½·10·6 = 30 kN
x̄ = L/3 = 2 m

Equilibrium

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

ΣMA = 0: RB·6 = 30·2
RB = 10 kN
RA = 30 − 10 = 20 kN

Answer

RA = 20 kN
2.Beam support reactions

Answer: MA = 368 kN·m

Cantilever equilibrium: a fixed support can push up and also resist rotation, so it gives a vertical reaction RA and a reaction moment MA. ΣFy = 0 gives RA, and moments about the wall give MA = Σ(load × distance from the wall). A distributed load acts as its resultant at the centroid of the load diagram.

Resultant of the triangular load

W = ½·12·8 = 48 kN
x̄ = L/3 = 2.667 m

Moment about the wall

MA = W·x̄ + P·a = 48·2.667 + 60·4 = 368 kN·m

Answer

MA = 368 kN·m
3.Truss: method of joints

Answer: FAB = −8.784 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 = 10·1 → Cy = 1.667 kN
ΣFy = 0: Ay = 10 − 1.667 = 8.333 kN

Joint A

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

sin α = 3/3.162 = 0.9487
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −8.333/0.9487 = −8.784 kN

Answer

FAB = −8.784 kN (compression)
4.Truss: method of joints

Answer: FAB = −34.14 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.

ABBCACACB55 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 55·1 + 30·4 → Cy = 21.88 kN
ΣFy = 0: Ay = 55 − 21.88 = 33.13 kN
ΣFx = 0: Ax = −30 kN

Joint A

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

sin α = 4/4.123 = 0.9701
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −33.13/0.9701 = −34.14 kN

Answer

FAB = −34.14 kN (compression)
5.Shear force & bending moment

Answer: E (x = 8 m)

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

Support reactions

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

R1 = 32.5 kN, R2 = 52.5 kN

Bending moment at every mark

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

MA = 0, MB = 65, MC = 130, MD = 195, ME = 210 kN·m, MF = 105, MG = 0

Answer

Mark E: ME = 210 kN·m
6.Shear force & bending moment

Answer: Mx = 93.75 kN·m

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

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 5·8 = 40 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 45·6 + 5·8·4
RB = 430/8 = 53.75 kN
ΣFy = 0: RA = 85 − 53.75 = 31.25 kN
w = 5 kN/mP = 45 kNABRA​ = 31.25RB​ = 53.75section5 m1 m2 m

Cut at x = 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 = 31.25·5 − 5·5·2.5 = 93.75 kN·m

Answer

Mx = 93.75 kN·m
7.Beam deflection

Answer: δmax = 44.56 mm

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition).

Consistent units

Work in N and mm: P in N, w in N/mm (kN/m = N/mm), L in mm, E in N/mm² (GPa × 1000), I in mm⁴.

w = 20 N/mm, L = 2000 mm
EI = 9.35 × 10¹⁰ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·20·2000⁴/(384·9.35 × 10¹⁰) = 44.56 mm

Answer

δmax = 44.56 mm
8.Beam deflection

Answer: δmax = 40.33 mm

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition).

Consistent units

Work in N and mm: P in N, w in N/mm (kN/m = N/mm), L in mm, E in N/mm² (GPa × 1000), I in mm⁴.

P = 16000 N, L = 5000 mm
EI = 1.76 × 10¹² N·mm²

One load at L/3

δ₁ = Pb(3L² − 4b²)/(48EI), b = L/3 = 1667 mm
δ₁ = 20.17 mm

Add both loads

δmax = 2·δ₁ = 23PL³/(648EI) = 40.33 mm

Answer

δmax = 40.33 mm
9.Column buckling

Answer: Pcr = 13.25 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·25⁴/64 = 19175 mm⁴

Effective length

KL = 0.5·2000 = 1000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·19175/1000² = 13247 N = 13.25 kN

Answer

Pcr = 13.25 kN
10.Column buckling

Answer: σcr = 5.483 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·80⁴/64 = 2.011 × 10⁶ mm⁴

Radius of gyration and slenderness

A = 5027 mm²
r = √(I/A) = √(2.011 × 10⁶/5027) = 20 mm
KL = 2·6000 = 12000 mm
KL/r = 12000/20 = 600

Critical stress

σcr = π²E/(KL/r)² = π²·200000/600² = 5.483 MPa

Answer

σcr = 5.483 MPa
11.Centroid & second moment of area

Answer: Ix = 24.35 × 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 − 2827·105)/(15000 − 2827) = 68.03 mm

Full plate about ȳ

100·150³/12 + 15000·6.968² = 28.85 × 10⁶ mm⁴

Hole about ȳ

π·60⁴/64 + 2827·36.97² = 4.5 × 10⁶ mm⁴

Subtract

Ix = 24.35 × 10⁶ mm⁴

Answer

Ix = 24.35 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 34.8 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 = 160 + 10/2 = 165 mm
web: Aw = 8·160 = 1280 mm², yw = 160/2 = 80 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2800·165 + 1280·80)/4080 = 138.3 mm

Parallel-axis theorem

flange: 280·10³/12 + 2800·(165 − 138.3)² = 2.014 × 10⁶ mm⁴
web: 8·160³/12 + 1280·(80 − 138.3)² = 7.086 × 10⁶ mm⁴
Ix = 2.014 × 10⁶ + 7.086 × 10⁶ = 9.101 × 10⁶ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 170 − 138.3 = 31.67 mm
σ = M·y/I = 1 × 10⁷·31.67/9.101 × 10⁶ = 34.8 MPa

Answer

σtop = 34.8 MPa
13.Effective stress in soil

Answer: u = 19.62 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) = 9.81·2 = 19.62 kPa

Answer

u = 19.62 kPa
14.Effective stress in soil

Answer: σ = 162 kPa

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

Total stress

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

σ = γd·3 + γsat,sand·3 + γsat,clay·3
σ = 16·3 + 19.5·3 + 18.5·3 = 162 kPa

Answer

σ = 162 kPa
15.Consolidation settlement

Answer: S = 181 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 + 160 = 265 kPa > 165 kPa

Settlement

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

S = 0.03·6/(1 + 0.9)·log₁₀(165/105) + 0.25·6/(1 + 0.9)·log₁₀(265/165)
S = 18.6 + 162.4 = 181 mm

Answer

S = 181 mm
16.Consolidation settlement

Answer: t = 880.2 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 = 20/2 = 10 mm = 0.01 m
Hdr,field = 6.5/2 = 3.25 m

Scale the time

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

tfield = 12·(3.25/0.01)² = 1.268 × 10⁶ min
tfield = 1.268 × 10⁶/1440 = 880.2 days

Answer

t = 880.2 days
17.Hydrostatic force

Answer: F = 55.18 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 + 2.5/2 = 2.25 m
A = H·b = 2.5·1 = 2.5 m²
gated = 1 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.25·2.5 = 55.18 kN

Answer

F = 55.18 kN
18.Hydrostatic force

Answer: ycp = 3.308 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 = 2.5 + 1.5/2 = 3.25 m
A = H·b = 1.5·1.5 = 2.25 m²
gated = 2.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.25·2.25 = 71.74 kN

Centre of pressure

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

Ic = b·H³/12 = 1.5·1.5³/12 = 0.4219 m⁴
ycp = yc + Ic/(yc·A) = 3.25 + 0.4219/(3.25·2.25) = 3.308 m

Answer

ycp = 3.308 m
19.Pipe friction & head loss

Answer: hf = 10.44 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 head

V²/(2g) = 1.6²/(2·9.81) = 0.1305 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.02·(1000/0.25)·1.6²/(2·9.81) = 10.44 m

Answer

hf = 10.44 m
20.Pipe friction & head loss

Answer: H = 3.384 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 = 0.08/0.04909 = 1.63 m/s
V²/(2g) = 0.1354 m

Loss coefficients

f·L/D = 0.022·200/0.25 = 17.6
ΣK = 0.5 + 3·0.3 + 5 = 6.4

Energy equation

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

H = (1 + 17.6 + 6.4)·0.1354 = 3.384 m

Answer

H = 3.384 m
21.Open-channel flow (Manning)

Answer: Q = 6.918 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 = 4.5·0.6 = 2.7 m²
P = b + 2y = 4.5 + 2·0.6 = 5.7 m
R = A/P = 0.4737 m

Velocity

V = (1/0.015)·0.47372/3·0.0041/2 = 2.562 m/s

Flow rate

Q = A·V = 2.7·2.562 = 6.918 m³/s

Answer

Q = 6.918 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.005091 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 = (2.5 + 2·0.6)·0.6 = 2.22 m²
P = b + 2y·√(1 + z²) = 2.5 + 2·0.6·√(1 + 2²) = 5.183 m
R = A/P = 0.4283 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.025·3.6/(2.22·0.5682) = 0.07135
S = 0.07135² = 0.005091

Answer

S = 0.005091

That is a fall of 5.091 m per kilometre.

23.Pumps & pump power

Answer: Pel = 22.15 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 = 1000·9.81·0.03·58 = 17.07 kW

Shaft power

Pshaft = 17.07/0.82 = 20.82 kW

Electrical power

Pel = 20.82/0.94 = 22.15 kW

Answer

Pel = 22.15 kW
24.Pumps & pump power

Answer: Pshaft = 8.117 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 = 0.02/0.007854 = 2.546 m/s
V²/(2g) = 0.3305 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (33 + 6)·0.3305 = 12.89 m

Pump head

H = Δz + hL = 14 + 12.89 = 26.89 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.02·26.89/0.65 = 8.117 kW

Answer

Pshaft = 8.117 kW
25.Time value of money

Answer: FV = 5773 €

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 = 0.048/12 = 0.004
N = m·n = 12·3 = 36

Future value

FV = 5 000·(1 + 0.004)36 = 5 000·1.155 = €5 772.76

Answer

FV = €5 772.76
26.Time value of money

Answer: I = 5189 €

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 = 72
A = 30 000·0.0045/(1 − (1 + 0.0045)−72) = €488.73

Total interest

I = N·A − P = 72·488.7 − 30 000 = €5 188.85

Answer

I = €5 188.85
27.NPV & IRR

Answer: NPV = −5938 €

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 = −60 000
CF1/(1 + 0.08)1 = 16 000/1.08 = 14 814.81
CF2/(1 + 0.08)2 = 18 000/1.166 = 15 432.10
CF3/(1 + 0.08)3 = 30 000/1.26 = 23 814.97

Add them up

NPV = €−5 938.12

Answer

NPV = €−5 938.12

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

28.NPV & IRR

Answer: IRR = 27.96 %

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%) = 1 888.00
NPV(30%) = −1 219.85

Narrow down

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

IRR ≈ 25 + 5·1 888.00/(1 888.00 − (−1 219.85)) = 28.04%
exact: NPV(27.96%) = 0 → IRR = 27.96%

Answer

IRR = 27.96%
29.Normal distribution

Answer: P = 0.2902

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 = (96.25 − 100)/15 = −0.25
z₂ = (107.5 − 100)/15 = 0.5

Area between

P = Φ(0.5) − Φ(−0.25) = 0.6915 − 0.4013 = 0.2902

Answer

P = 0.2902
30.Normal distribution

Answer: x = 434 h

From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.

Area to the left

Φ(z) = 0.05

z from the table

z ≈ −1.64

Back to the original units

x = 500 − 1.64·40 = 434 h

Answer

x = 434 h

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