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​ = 12 kN/mP = 80 kNABRB​ = ?3 m7 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that falls from 12 kN/m at A to zero at B. A point load P also acts at 3 m from A. Find the vertical support reaction RB.

L = 10 mw0 = 12 kN/mP = 80 kN at 3 m
RB = kN
2.Beam support reactionsHard
w0​ = 4 kN/mP = 40 kNABMA​ = ?3 m5 m

The cantilever beam is fixed to the wall at A. It carries a linearly varying load that is 4 kN/m at the wall and falls to zero at the free end B, plus a point load P at 3 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 8 mw0 = 4 kN/mP = 40 kN at 3 m
MA = kN·m
3.Truss: method of jointsMedium
ABBCACACB25 kN8 m3 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 3 m from Avertical load = 25 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB20 kN5 kN8 m3 m4 m

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

span = 8 mheight = 4 mB is 3 m from Avertical load = 20 kNhorizontal load = 5 kN ←
FBC = kN
5.Shear force & bending momentMedium
P1​ = 75 kNP2​ = 30 kNABC1 m4 m2 m

The beam rests on a pin at A and a roller at B and overhangs B by 2 m to the free end C. It carries a point load P1 between the supports and a point load P2 at C. Find the bending moment Mx under the load P1. Use sagging moments positive and upward shear on the left face positive.

L = 7 mP1 = 75 kN at 1 mP2 = 30 kN at 7 msupports at x = 0 and x = 5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 2 kN/mP = 20 kNABsection0.5 m2.5 m1 m

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

L = 4 mP = 20 kN at 3 mw = 2 kN/m from 0 to 4 mx = 0.5 m
Mx = kN·m
7.Beam deflectionMedium
P = 21 kNABδ0.5 m2.5 m

A cantilever of length L is fixed at A and carries a point load P at a distance a = 0.5 m from A. Find the deflection δB at the free end B.

P = 21 kNa = 0.5 mL = 3 mE = 70 GPa (aluminium)I = 36 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
P = 16 kNP = 16 kNABδ1.333 m1.334 m1.333 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 = 4 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 5 m30 × 60 mmcross-section

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

L = 5 mE = 70 GPa (aluminium)b × h = 30 × 60 mm
Pcr = kN
10.Column bucklingHard
P = 85 kNL = 1.5 md = ?cross-section

A solid round column of length L made of steel is pinned at both ends. It must carry 85 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 85 kNn = 3L = 1.5 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
2802028018xdimensions in mm

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

bf = 280 mmtf = 20 mmtw = 18 mmhw = 280 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
150 mm200 mm140 mm80 × 20xIx​ = ?

A 150 mm × 200 mm plate has a rectangular cut-out 80 mm wide and 20 mm high, centred on the vertical centre line with its centre 140 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 150 mmh = 200 mmcut-out: 80 × 20 mmhole centre: y = 140 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 20 kN/m³10 mwater tableXz = 6 m

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

z = 6 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 20 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 18.5 kN/m³4 mclayγsat​ = 17 kN/m³7 mwater tableXz = 7.5 m

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

z = 7.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 18.5 kN/m³clay: γsat = 17 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 15 kPasandclayCc​ = 0.45, Cr​ = 0.05e0​ = 1σ′0​ = 90 kPaσ′p​ = 150 kPa7 mwater table

A 7 m thick overconsolidated clay layer has Cc = 0.45, Cr = 0.05 and e₀ = 1. At its mid-depth the effective vertical stress is 90 kPa and the preconsolidation pressure is 150 kPa. A new building adds 15 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7 mCc = 0.45Cr = 0.05e0 = 1σ′0 = 90 kPaσ′p = 150 kPaΔσ = 15 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 3 mcv​ = 5 m²/year3 msandwater table

A clay layer 3 m thick has a coefficient of consolidation cv = 5 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 = 3 mcv = 5 m²/yearU = 90%Tv = 0.848double drainage
t = years
17.Hydrostatic forceMedium
gated = 0.5 mH = 2.5 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 0.5 mH = 2.5 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 4 mH = 2 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of glycerin, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 2 mb = 1 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1.6 m/sD = 200 mmL = 400 mf = 0.028

Water flows at a mean velocity of 1.6 m/s through a pipe 400 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.028 and g = 9.81 m/s². Find the friction head loss hf.

V = 1.6 m/sL = 400 mD = 200 mmf = 0.028g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5Δz = 24 mL = 100 m, D = 150 mm, f = 0.0222× bend (K = 0.3)

Two open reservoirs are joined by a pipe 100 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.022. The water surface of the upper reservoir is 24 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each), a valve (K = 5) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². Find the flow rate Q in L/s.

Δz = 24 mL = 100 mD = 150 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 5Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 3 my = 1 mn = 0.03, S = 0.001

A rectangular grass-lined earth channel is 3 m wide. Water flows uniformly 1 m deep. Manning n = 0.03 and the bed slope is S = 0.001. Find the flow rate Q in m³/s.

b = 3 my = 1 mn = 0.03S = 0.001
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 1.5 my = 0.7 m1.5 : 1n = 0.025, Q = 2.9 m³/s

A trapezoidal gravel channel with a bottom width of 1.5 m and side slopes of 1.5:1 (horizontal:vertical) must carry 2.9 m³/s in uniform flow at a depth of 0.7 m. Manning n = 0.025. Find the required bed slope S (in m/m).

Q = 2.9 m³/sb = 1.5 my = 0.7 mz = 1.5n = 0.025
S = m/m
23.Pumps & pump powerMedium
PQ = 150 L/sH = 78 m

A pump with an efficiency of 60% delivers 150 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 = 150 L/sH = 78 mη = 60%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 50 L/sΔz = 5 mL = 300 m, D = 150 mm, f = 0.02, ΣK = 4

A pump moves 50 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 5 m higher. The pipe is 300 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 4 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 80%. Find the shaft power Pshaft in kW.

Q = 50 L/sΔz = 5 mL = 300 mD = 150 mmf = 0.02ΣK = 4η = 80%
Pshaft = kW
25.Time value of moneyMedium
periods0123…1211 + EAR = ?16% / 12

A credit card charges a nominal interest rate of 16% per year, compounded monthly. Find the effective annual rate EAR in percent.

r = 16%m = 12
EAR = %
26.Time value of moneyHard
years0123…27€2 500€2 500€2 500FV = ?

You deposit €2 500 at the start of every year for 27 years, the first deposit today. The account pays 4% per year. How much is in the account at the end of year 27? Find FV.

A = €2 500i = 4%n = 27
FV = €
27.NPV & IRRMedium
years01234−20 0008 0005 0009 0005 000

An investment of €20 000 gives these cash flows at the end of years 1 to 4: €8 000, €5 000, €9 000, €5 000. The cost of capital is 15%. Find the net present value NPV.

r = 15%CF0 = −20 000CF1 = 8 000CF2 = 5 000CF3 = 9 000CF4 = 5 000
NPV = €
28.NPV & IRRHard
years012−40 00027 50028 500

A project costs €40 000 and returns €27 500, €28 500 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 27 500CF2 = 28 500
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area between −z and z = 0.8098

Drag z so that the shaded area between −z and z under the standard normal curve is 0.8098. Find z to two decimals.

A = 0.8098
z =
30.Normal distributionHard
0.04 mm0D − d?

Hole diameters D are normal with mean 25.04 mm and standard deviation 0.015 mm. Shaft diameters d are independent and normal with mean 25 mm and standard deviation 0.02 mm. A randomly chosen shaft fits when D − d > 0. Find the probability P that it fits. Round z to two decimals.

hole: μ = 25.04 mm, σ = 0.015 mmshaft: μ = 25 mm, σ = 0.02 mm
P =

3Solutions

1.Beam support reactions

Answer: RB = 44 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 = ½·12·10 = 60 kN
x̄ = L/3 = 3.333 m

Equilibrium

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

ΣMA = 0: RB·10 = 60·3.333 + 80·3
RB = 44 kN
RA = 140 − 44 = 96 kN

Answer

RB = 44 kN
2.Beam support reactions

Answer: MA = 162.7 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 = ½·4·8 = 16 kN
x̄ = L/3 = 2.667 m

Moment about the wall

MA = W·x̄ + P·a = 16·2.667 + 40·3 = 162.7 kN·m

Answer

MA = 162.7 kN·m
3.Truss: method of joints

Answer: FAB = −19.53 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·8 = 25·3 → Cy = 9.375 kN
ΣFy = 0: Ay = 25 − 9.375 = 15.63 kN

Joint A

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

sin α = 4/5 = 0.8
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −15.63/0.8 = −19.53 kN

Answer

FAB = −19.53 kN (compression)
4.Truss: method of joints

Answer: FBC = −8.004 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.

ABBCACACB20 kN5 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 20·3 − 5·4 → Cy = 5 kN
ΣFy = 0: Ay = 20 − 5 = 15 kN
ΣFx = 0: Ax = 5 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 = 4/6.403 = 0.6247, cos γ = 5/6.403 = 0.7809
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −5/0.6247 = −8.004 kN

Answer

FBC = −8.004 kN (compression)
5.Shear force & bending moment

Answer: Mx = 48 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. The overhang load also acts about A.

ΣMA = 0: RB·5 = 75·1 + 30·7
RB = 285/5 = 57 kN
ΣFy = 0: RA = 105 − 57 = 48 kN

Cut under P1 and keep the left part

Mx = RA·1 = 48·1 = 48 kN·m

Answer

Mx = 48 kN·m
6.Shear force & bending moment

Answer: Mx = 4.25 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 = 2·4 = 8 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 20·3 + 2·4·2
RB = 76/4 = 19 kN
ΣFy = 0: RA = 28 − 19 = 9 kN
w = 2 kN/mP = 20 kNABRA​ = 9RB​ = 19section0.5 m2.5 m1 m

Cut at x = 0.5 m and keep the left part

Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 9·0.5 − 2·0.5·0.25 = 4.25 kN·m

Answer

Mx = 4.25 kN·m
7.Beam deflection

Answer: δB = 2.951 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 = 21000 N, a = 500 mm, L = 3000 mm
EI = 2.52 × 10¹² N·mm²

Deflection at the free end

Deflection at the load plus the slope at the load times the remaining length.

δP = Pa³/(3EI) = 0.3472 mm
θP = Pa²/(2EI) = 0.001042 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 2.951 mm

Answer

δB = 2.951 mm
8.Beam deflection

Answer: δmax = 15.14 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 = 4000 mm
EI = 2.4 × 10¹² N·mm²

One load at L/3

δ₁ = Pb(3L² − 4b²)/(48EI), b = L/3 = 1333 mm
δ₁ = 7.572 mm

Add both loads

δmax = 2·δ₁ = 23PL³/(648EI) = 15.14 mm

Answer

δmax = 15.14 mm
9.Column buckling

Answer: Pcr = 3.731 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 = 60·30³/12 = 135000 mm⁴

Effective length

KL = 1·5000 = 5000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·135000/5000² = 3731 N = 3.731 kN

Answer

Pcr = 3.731 kN
10.Column buckling

Answer: d = 49.33 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 = 3·85000 = 255000 N
KL = 1·1500 = 1500 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·255000·1500²/(π³·200000))^(1/4) = 49.33 mm

Answer

d = 49.33 mm

Check: the slenderness KL/r is 121.6, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 92.8 × 10⁶ mm⁴

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

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 280·20 = 5600 mm², yf = 280 + 20/2 = 290 mm
web: Aw = 18·280 = 5040 mm², yw = 280/2 = 140 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (5600·290 + 5040·140)/10640 = 218.9 mm

Parallel-axis theorem

flange: 280·20³/12 + 5600·(290 − 218.9)² = 2.846 × 10⁷ mm⁴
web: 18·280³/12 + 5040·(140 − 218.9)² = 6.434 × 10⁷ mm⁴
Ix = 2.846 × 10⁷ + 6.434 × 10⁷ = 9.28 × 10⁷ mm⁴ = 92.8 × 10⁶ mm⁴

Answer

Ix = 92.8 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 97.24 × 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 = (30000·100 − 1600·140)/(30000 − 1600) = 97.75 mm

Full plate about ȳ

150·200³/12 + 30000·2.254² = 100.2 × 10⁶ mm⁴

Hole about ȳ

80·20³/12 + 1600·42.25² = 2.91 × 10⁶ mm⁴

Subtract

Ix = 97.24 × 10⁶ mm⁴

Answer

Ix = 97.24 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ′ = 67.45 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) = 16.5·1 + 20·5 = 116.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·5 = 49.05 kPa

Effective stress

σ′ = σ − u = 116.5 − 49.05 = 67.45 kPa

Answer

σ′ = 67.45 kPa
14.Effective stress in soil

Answer: σ = 128.5 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·2 + γsat,sand·2 + γsat,clay·3.5
σ = 16·2 + 18.5·2 + 17·3.5 = 128.5 kPa

Answer

σ = 128.5 kPa
15.Consolidation settlement

Answer: S = 11.72 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 = 90 + 15 = 105 kPa ≤ 150 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·7/(1 + 1)·log₁₀(105/90) = 11.72 mm

Answer

S = 11.72 mm
16.Consolidation settlement

Answer: t = 0.3816 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 = 3/2 = 1.5 m

Time

t = Tv·Hdr²/cv = 0.848·1.5²/5 = 0.3816 years

Answer

t = 0.3816 years
17.Hydrostatic force

Answer: F = 64.38 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 = 0.5 + 2.5/2 = 1.75 m
A = H·b = 2.5·1.5 = 3.75 m²
gated = 0.5 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·1.75·3.75 = 64.38 kN

Answer

F = 64.38 kN
18.Hydrostatic force

Answer: F = 123.6 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 = 4 + 2/2 = 5 m
A = H·b = 2·1 = 2 m²
gated = 4 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·5·2 = 123.6 kN

Answer

F = 123.6 kN
19.Pipe friction & head loss

Answer: hf = 7.307 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) = 0.028·(400/0.2)·1.6²/(2·9.81) = 7.307 m

Answer

hf = 7.307 m
20.Pipe friction & head loss

Answer: Q = 82.19 L/s

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.

Loss coefficients

f·L/D = 0.022·100/0.15 = 14.67
ΣK = 0.5 + 2·0.3 + 5 + 1.0 = 7.1

Energy equation

Both surfaces are open to the air and practically at rest, so all of Δz is lost in the pipe.

24 = (14.67 + 7.1)·V²/(2·9.81)
V = √(2·9.81·24/21.77) = 4.651 m/s

Flow rate

Q = V·π·D²/4 = 4.651·0.01767 = 0.08219 m³/s = 82.19 L/s

Answer

Q = 82.19 L/s
21.Open-channel flow (Manning)

Answer: Q = 2.25 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 = 3·1 = 3 m²
P = b + 2y = 3 + 2·1 = 5 m
R = A/P = 0.6 m

Velocity

V = (1/0.03)·0.62/3·0.0011/2 = 0.7499 m/s

Flow rate

Q = A·V = 3·0.7499 = 2.25 m³/s

Answer

Q = 2.25 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.004876 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 = (1.5 + 1.5·0.7)·0.7 = 1.785 m²
P = b + 2y·√(1 + z²) = 1.5 + 2·0.7·√(1 + 1.5²) = 4.024 m
R = A/P = 0.4436 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.025·2.9/(1.785·0.5816) = 0.06983
S = 0.06983² = 0.004876

Answer

S = 0.004876

That is a fall of 4.876 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 191.3 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 = 1000·9.81·0.15·78 = 114.8 kW

Shaft power

Pshaft = Ph/η = 114.8/0.6 = 191.3 kW

Answer

Pshaft = 191.3 kW
24.Pumps & pump power

Answer: Pshaft = 14.07 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 = 0.05/0.01767 = 2.829 m/s
V²/(2g) = 0.408 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (40 + 4)·0.408 = 17.95 m

Pump head

H = Δz + hL = 5 + 17.95 = 22.95 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.05·22.95/0.8 = 14.07 kW

Answer

Pshaft = 14.07 kW
25.Time value of money

Answer: EAR = 17.23 %

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 per period

r/m = 0.16/12 = 0.01333

Compound over one year

EAR = (1 + 0.01333)12 − 1 = 1.172 − 1 = 17.23%

Answer

EAR = 17.23%

The EAR is always above the nominal rate when interest compounds more than once a year.

26.Time value of money

Answer: FV = 122419 €

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.

Ordinary annuity factor

((1 + 0.04)27 − 1)/0.04 = 47.08

Annuity due

Each deposit is invested one year longer.

FV = 2 500·47.08·1.04 = €122 418.96

Answer

FV = €122 418.96
27.NPV & IRR

Answer: NPV = −486.3 €

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 = −20 000
CF1/(1 + 0.15)1 = 8 000/1.15 = 6 956.52
CF2/(1 + 0.15)2 = 5 000/1.322 = 3 780.72
CF3/(1 + 0.15)3 = 9 000/1.521 = 5 917.65
CF4/(1 + 0.15)4 = 5 000/1.749 = 2 858.77

Add them up

NPV = €−486.35

Answer

NPV = €−486.35

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

28.NPV & IRR

Answer: IRR = 25.52 %

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%) = 240.00
NPV(30%) = −1 982.25

Narrow down

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

IRR ≈ 25 + 5·240.00/(240.00 − (−1 982.25)) = 25.54%
exact: NPV(25.52%) = 0 → IRR = 25.52%

Answer

IRR = 25.52%
29.Normal distribution

Answer: z = 1.31

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 of z

Φ(z) = (1 + 0.8098)/2 = 0.9049

Read the z-table backwards

Find 0.9049 inside the table and read off z.

z = 1.31

Answer

z = 1.31
30.Normal distribution

Answer: P = 0.9452

Sums and differences of normal variables: if X and Y are independent and normal, X + Y and X − Y are normal too. Means add or subtract: E(X ± Y) = μX ± μY. Variances always add, also for a difference: Var(X ± Y) = σX² + σY², so σ = √(σX² + σY²). Standard deviations never add directly. The total of n independent items with the same distribution has mean n·μ and standard deviation σ·√n. Then standardise as usual: z = (x − mean)/σ and read Φ(z).

Distribution of the difference

μ = 25.04 − 25 = 0.04 mm, σ = 0.025 mm

Standardise

z = (0 − 0.04)/0.025 = −1.6

Probability

P = 1 − Φ(−1.6) = 0.9452

Answer

P = 0.9452

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