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​ = 30 kNP2​ = 15 kNABRA​ = ?RB​2 m3 m3 m

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

L = 8 mP1 = 30 kN at 2 mP2 = 15 kN at 5 m
RA = kN
2.Beam support reactionsHard
P = 10 kNQ = 45 kNADCMA​ = ?5 m1 m3 m1 m

A compound beam is fixed to the wall at A, has an internal hinge at C (6 m from A) and rests on a roller at D (10 m from A). It carries a point load P at 9 m from A and a point load Q at 5 m from A. Find the magnitude of the reaction moment MA at the wall.

AC = 6 mAD = 10 mP = 10 kN at 9 mQ = 45 kN at 5 m
MA = kN·m
3.Truss: method of jointsMedium
ABBCACACB55 kN8 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 = 8 mheight = 3 mB is 1 m from Avertical load = 55 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB35 kN20 kN8 m1 m3 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 = 3 mB is 1 m from Avertical load = 35 kNhorizontal load = 20 kN ←
FBC = kN
5.Shear force & bending momentMedium
5 kN/m60 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 @ 6 m5 kN/m, 0–12 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 = 2 kN/mABC6 m1 m

The beam rests on a pin at A and a roller at B and overhangs B by 1 m to the free end C. A uniformly distributed load w acts over the whole length A–C. Find the maximum sagging bending moment Mmax between the supports.

L = 7 mw = 2 kN/m from 0 to 7 msupports at x = 0 and x = 6 m
Mmax = kN·m
7.Beam deflectionMedium
P = 12 kNABδ4 m2 m

A simply supported beam carries a point load P at a = 4 m from support A. Find the deflection δP under the load.

P = 12 kNa = 4 mL = 6 mE = 70 GPa (aluminium)I = 160 × 10⁶ mm⁴
δP = mm
8.Beam deflectionHard
w = 6 kN/mP = 24 kNδL = 2 m

A simply supported beam carries a uniformly distributed load w and a point load P at midspan. Using superposition, find the midspan deflection δmax.

P = 24 kNw = 6 kN/mL = 2 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 3 m30 × 100 mmcross-section

A column of length L made of steel is fixed at the base and free at the top. Using Euler’s formula, find its critical buckling load Pcr.

L = 3 mE = 200 GPa (steel)b × h = 30 × 100 mm
Pcr = kN
10.Column bucklingHard
PL = 2.5 md = 60 mmcross-section

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

L = 2.5 mE = 70 GPa (aluminium)d = 60 mm
σcr = MPa
11.Centroid & second moment of areaMedium
280130t = 18ȳ = ?dimensions in mm

A channel section lies with its open side up: a base plate 280 mm wide with two upright legs, 130 mm high overall. Base and legs are all 18 mm thick. Find the height ȳ of the centroid above the bottom edge.

b = 280 mmh = 130 mmt = 18 mm
ȳ = mm
12.Centroid & second moment of areaHard
1904801414xM = 50 kN·mdimensions in mm

A symmetric I-section has flanges 190 mm wide and 14 mm thick, an overall depth of 480 mm and a web 14 mm thick. It carries a bending moment of 50 kN·m about the axis x. Find the size of the bending stress σj at the junction of the web and the top flange.

B = 190 mmH = 480 mmtf = 14 mmtw = 14 mmM = 50 kN·m
σj = MPa
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 20 kN/m³13 mwater tableXz = 9 m

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

z = 9 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20 kN/m³
σ = kPa
14.Effective stress in soilHard
sandγd​ = 16.5 kN/m³γsat​ = 19.5 kN/m³4 mclayγsat​ = 19 kN/m³6 mwater tableXz = 7 m

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

z = 7 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19.5 kN/m³clay: γsat = 19 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 120 kPasandclayCc​ = 0.5, Cr​ = 0.06e0​ = 0.6σ′0​ = 95 kPaOCR = 32 mwater table

A 2 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.06 and e₀ = 0.6. At its mid-depth the effective vertical stress is 95 kPa and the overconsolidation ratio is OCR = 3. A new building adds 120 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2 mCc = 0.5Cr = 0.06e0 = 0.6σ′0 = 95 kPaOCR = 3Δσ = 120 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 10 mcv​ = 1 m²/year10 msandwater table

A clay layer 10 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 = 10 mcv = 1 m²/yearU = 90%Tv = 0.848double drainage
t = years
17.Hydrostatic forceMedium
gated = 1 mH = 3 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 = 3 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 3 mH = 1.5 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of glycerin, with its top edge 3 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 3 mH = 1.5 mb = 3 mρ = 1260 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 2.5 m/sD = 150 mmL = 1000 mf = 0.02

Water flows at a mean velocity of 2.5 m/s through a pipe 1000 m long with an inside diameter of 150 mm. Use the Darcy friction factor f = 0.02 and g = 9.81 m/s². Find the friction head loss hf.

V = 2.5 m/sL = 1000 mD = 150 mmf = 0.02g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5Δz = ?L = 150 m, D = 100 mm, f = 0.023× bend (K = 0.3)

Two open reservoirs are joined by a pipe 150 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.02. The minor losses are a square-edged entrance (K = 0.5), 3 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. What difference in water level Δz between the reservoirs gives a flow rate of 25 L/s?

Q = 25 L/sL = 150 mD = 100 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
D = 600 mmn = 0.013, S = 0.002

A concrete storm sewer with an inside diameter of 600 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.002. Find the flow rate Q in m³/s.

D = 600 mmn = 0.013S = 0.002
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 5.5 my = 1.1 mn = 0.022, Q = 10 m³/s

A rectangular clean earth channel 5.5 m wide must carry 10 m³/s in uniform flow at a depth of 1.1 m. Manning n = 0.022. Find the required bed slope S (in m/m).

Q = 10 m³/sb = 5.5 my = 1.1 mn = 0.022
S = m/m
23.Pumps & pump powerMedium
PQ = 60 L/sH = 70 m

In a test, a pump delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 70 m while its shaft takes 58.9 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 60 L/sH = 70 mPshaft = 58.9 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 120 L/sΔz = 24 mL = 600 m, D = 250 mm, f = 0.022, ΣK = 8

A pump moves 120 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 24 m higher. The pipe is 600 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.022; 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 = 120 L/sΔz = 24 mL = 600 mD = 250 mmf = 0.022ΣK = 8
H = m
25.Time value of moneyMedium
years0123…9PV = ?€20 000+3%+3%…r = 7%

A property is expected to earn net rent of €20 000 next year. The rent is expected to grow by 3% per year forever. The required return is 7% per year. Find the value PV of the property today.

C1 = €20 000g = 3%r = 7%
PV = €
26.Time value of moneyHard
months0123…N = ?€25 000€325€325€325€3254.2% / 12

You borrow €25 000 at 4.2% per year, compounded monthly, and repay €325 at the end of every month. How many months does it take until the loan is repaid (the last payment may be smaller)? Give the number of payments N.

P = €25 000A = €3254.2% / 12
N = payments
27.NPV & IRRMedium
years01234−60 00014 00020 00021 00018 000

An investment of €60 000 gives these cash flows at the end of years 1 to 4: €14 000, €20 000, €21 000, €18 000. The cost of capital is 8%. Find the net present value NPV.

r = 8%CF0 = −60 000CF1 = 14 000CF2 = 20 000CF3 = 21 000CF4 = 18 000
NPV = €
28.NPV & IRRHard
years012−25 00014 50018 000

A project costs €25 000 and returns €14 500, €18 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −25 000CF1 = 14 500CF2 = 18 000
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area to the right of z = 0.0136

Drag z so that the shaded area under the standard normal curve, to the right of z, is 0.0136. Find z to two decimals.

A = 0.0136
z =
30.Normal distributionHard
380420460500540580620htop 70%

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. Drag the cut-off so the shaded top 70% is to the right of it. Find the cut-off x.

μ = 500 hσ = 40 h70%
x = h

3Solutions

1.Beam support reactions

Answer: RA = 28.13 kN

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

P1​ = 30 kNP2​ = 15 kNABRA​RB​2 m3 m3 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·8 = 30·2 + 15·5
RB = 135/8 = 16.88 kN
ΣFy = 0: RA = 45 − 16.88 = 28.13 kN

Answer

RA = 28.13 kN
2.Beam support reactions

Answer: MA = 240 kN·m

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. An internal hinge cannot carry a bending moment, which gives one extra equation: the moment about the hinge of the forces on either side is zero.

Part CD

The hinge has no moment, so moments about C on CD alone must balance.

ΣMC = 0: RD·4 = 10·3
RD = 7.5 kN
VC = 10 − 7.5 = 2.5 kN

Part AC

The hinge force VC acts downward on AC (equal and opposite to its action on CD).

RA = 45 + 2.5 = 47.5 kN
MA = 45·5 + 2.5·6 = 240 kN·m

Answer

MA = 240 kN·m
3.Truss: method of joints

Answer: FAB = −50.73 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 55·1 → Cy = 6.875 kN
ΣFy = 0: Ay = 55 − 6.875 = 48.13 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 = −48.13/0.9487 = −50.73 kN

Answer

FAB = −50.73 kN (compression)
4.Truss: method of joints

Answer: FBC = 7.933 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.

ABBCACACB35 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 35·1 − 20·3 → Cy = −3.125 kN
ΣFy = 0: Ay = 35 − −3.125 = 38.13 kN
ΣFx = 0: Ax = 20 kN

Joint C

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

sin γ = 3/7.616 = 0.3939, cos γ = 7/7.616 = 0.9191
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −−3.125/0.3939 = 7.933 kN

Answer

FBC = 7.933 kN (tension)
5.Shear force & bending moment

Answer: D (x = 6 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 = 60 kN, R2 = 60 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 = 110, MC = 200, MD = 270 kN·m, ME = 200, MF = 110, MG = 0

Answer

Mark D: MD = 270 kN·m
6.Shear force & bending moment

Answer: Mmax = 8.507 kN·m

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

Support reactions

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

UDL resultant: W = w·ℓ = 2·7 = 14 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·6 = 2·7·3.5
RB = 49/6 = 8.167 kN
ΣFy = 0: RA = 14 − 8.167 = 5.833 kN

Zero shear

RA − w·x0 = 0 → x0 = 5.833/2 = 2.917 m

Maximum sagging moment

Mmax = RA·x0 − w·x0²/2 = RA²/(2w) = 5.833²/(2·2) = 8.507 kN·m

Answer

Mmax = 8.507 kN·m
7.Beam deflection

Answer: δP = 3.81 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 = 12000 N, a = 4000 mm, b = 2000 mm, L = 6000 mm
EI = 1.12 × 10¹³ N·mm²

Deflection under the load

δP = Pa²b²/(3EIL) = 12000·4000²·2000²/(3·1.12 × 10¹³·6000) = 3.81 mm

Answer

δP = 3.81 mm
8.Beam deflection

Answer: δmax = 2.188 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 = 24000 N, w = 6 N/mm, L = 2000 mm, EI = 2.4 × 10¹² N·mm²

Each load on its own

δP = PL³/(48EI) = 24000·2000³/(48·2.4 × 10¹²) = 1.667 mm
δw = 5wL⁴/(384EI) = 5·6·2000⁴/(384·2.4 × 10¹²) = 0.5208 mm

Add them

δmax = 1.667 + 0.5208 = 2.188 mm

Answer

δmax = 2.188 mm
9.Column buckling

Answer: Pcr = 12.34 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 = 100·30³/12 = 225000 mm⁴

Effective length

KL = 2·3000 = 6000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·225000/6000² = 12337 N = 12.34 kN

Answer

Pcr = 12.34 kN
10.Column buckling

Answer: σcr = 6.218 MPa

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

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·60⁴/64 = 636173 mm⁴

Radius of gyration and slenderness

A = 2827 mm²
r = √(I/A) = √(636173/2827) = 15 mm
KL = 2·2500 = 5000 mm
KL/r = 5000/15 = 333.3

Critical stress

σcr = π²E/(KL/r)² = π²·70000/333.3² = 6.218 MPa

Answer

σcr = 6.218 MPa
11.Centroid & second moment of area

Answer: ȳ = 37.89 mm

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

Split into rectangles

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

base: A1 = 280·18 = 5040 mm², y1 = 9 mm
two legs: A2 = 2·18·112 = 4032 mm², y2 = 18 + 112/2 = 74 mm

Centroid

ȳ = (5040·9 + 4032·74)/9072 = 37.89 mm

Answer

ȳ = 37.89 mm
12.Centroid & second moment of area

Answer: σj = 28.49 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.

Outer rectangle minus the two side cut-outs

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

hw = 480 − 2·14 = 452 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (190·480³ − 176·452³)/12
Ix = 3.966 × 10⁸ mm⁴

Bending stress

y = 240 − 14 = 226 mm
σ = M·y/I = 5 × 10⁷·226/3.966 × 10⁸ = 28.49 MPa

Answer

σj = 28.49 MPa
13.Effective stress in soil

Answer: σ = 176 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) = 16·1 + 20·8 = 176 kPa

Answer

σ = 176 kPa
14.Effective stress in soil

Answer: u = 39.24 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) = 9.81·4 = 39.24 kPa

Answer

u = 39.24 kPa
15.Consolidation settlement

Answer: S = 26.6 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.

Preconsolidation pressure

σ′p = OCR·σ′0 = 3·95 = 285 kPa

Compare with the preconsolidation pressure

σ′f = 95 + 120 = 215 kPa ≤ 285 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.06·2/(1 + 0.6)·log₁₀(215/95) = 26.6 mm

Answer

S = 26.6 mm
16.Consolidation settlement

Answer: t = 21.2 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 = 10/2 = 5 m

Time

t = Tv·Hdr²/cv = 0.848·5²/1 = 21.2 years

Answer

t = 21.2 years
17.Hydrostatic force

Answer: F = 73.58 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 + 3/2 = 2.5 m
A = H·b = 3·1 = 3 m²
gated = 1 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.5·3 = 73.58 kN

Answer

F = 73.58 kN
18.Hydrostatic force

Answer: ycp = 3.8 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 = 3 + 1.5/2 = 3.75 m
A = H·b = 1.5·3 = 4.5 m²
gated = 3 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·3.75·4.5 = 208.6 kN

Centre of pressure

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

Ic = b·H³/12 = 3·1.5³/12 = 0.8438 m⁴
ycp = yc + Ic/(yc·A) = 3.75 + 0.8438/(3.75·4.5) = 3.8 m

Answer

ycp = 3.8 m
19.Pipe friction & head loss

Answer: hf = 42.47 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) = 2.5²/(2·9.81) = 0.3186 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.02·(1000/0.15)·2.5²/(2·9.81) = 42.47 m

Answer

hf = 42.47 m
20.Pipe friction & head loss

Answer: Δz = 19.31 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 = 0.025/0.007854 = 3.183 m/s
V²/(2g) = 0.5164 m

Loss coefficients

f·L/D = 0.02·150/0.1 = 30
ΣK = 0.5 + 3·0.3 + 5 + 1.0 = 7.4

Total head loss

hf = 30·0.5164 = 15.49 m
hm = 7.4·0.5164 = 3.821 m
Δz = hf + hm = 19.31 m

Answer

Δz = 19.31 m
21.Open-channel flow (Manning)

Answer: Q = 0.2746 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 = 0.2827 m², R = D/4 = 0.15 m

Velocity

V = (1/0.013)·0.152/3·0.0021/2 = 0.9712 m/s

Flow rate

Q = A·V = 0.2827·0.9712 = 0.2746 m³/s

Answer

Q = 0.2746 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.001824 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·y = 5.5·1.1 = 6.05 m²
P = b + 2y = 5.5 + 2·1.1 = 7.7 m
R = A/P = 0.7857 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.022·10/(6.05·0.8515) = 0.04271
S = 0.04271² = 0.001824

Answer

S = 0.001824

That is a fall of 1.824 m per kilometre.

23.Pumps & pump power

Answer: η = 69.95 %

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.06·70 = 41.2 kW

Efficiency

η = Ph/Pshaft = 41.2/58.9 = 69.95%

Answer

η = 69.95%
24.Pumps & pump power

Answer: H = 42.52 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (52.8 + 8)·0.3046 = 18.52 m

Pump head

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

H = Δz + hL = 24 + 18.52 = 42.52 m

Answer

H = 42.52 m
25.Time value of money

Answer: PV = 500000 €

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.

Growing perpetuity

PV = C1/(r − g) = 20 000/(0.07 − 0.03) = 20 000/0.04 = €500 000.00

Answer

PV = €500 000.00
26.Time value of money

Answer: N = 90 payments

Time value of money: money today is worth more than the same amount later, because it can earn interest. With interest rate i per period, an amount grows as FV = PV·(1 + i)n. A series of equal payments (an annuity) is valued by adding up each payment, which gives the annuity formulas.

Rearrange the annuity formula

i = 0.0035
(1 + i)−N = 1 − 25 000·0.0035/325 = 0.7308

Solve with logarithms

N = −ln(0.7308)/ln(1.004) = 89.77

Round up to whole payments

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

N = 90

Answer

N = 90 payments
27.NPV & IRR

Answer: NPV = 10.75 €

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 = 14 000/1.08 = 12 962.96
CF2/(1 + 0.08)2 = 20 000/1.166 = 17 146.78
CF3/(1 + 0.08)3 = 21 000/1.26 = 16 670.48
CF4/(1 + 0.08)4 = 18 000/1.36 = 13 230.54

Add them up

NPV = €10.75

Answer

NPV = €10.75

NPV is positive, so the project earns more than the required return.

28.NPV & IRR

Answer: IRR = 18.67 %

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(15%) = 1 219.28
NPV(20%) = −416.67

Narrow down

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

IRR ≈ 15 + 5·1 219.28/(1 219.28 − (−416.67)) = 18.73%
exact: NPV(18.67%) = 0 → IRR = 18.67%

Answer

IRR = 18.67%
29.Normal distribution

Answer: z = 2.21

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 − 0.0136 = 0.9864

Read the z-table backwards

Find 0.9864 inside the table and read off z.

z = 2.21

Answer

z = 2.21
30.Normal distribution

Answer: x = 479 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) = 0.3

z from the table

z ≈ −0.52

Back to the original units

x = 500 − 0.52·40 = 479 h

Answer

x = 479 h

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