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​ = 55 kNP2​ = 45 kNABRA​ = ?RB​2 m5 m1 m

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

L = 8 mP1 = 55 kN at 2 mP2 = 45 kN at 7 m
RA = kN
2.Beam support reactionsHard
w = 2 kN/mP = 55 kNABRA​RB​ = ?1 m3 m4 m

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

L = 8 mP = 55 kN at 4 mw = 2 kN/m from 1 to 4 m
RB = kN
3.Truss: method of jointsMedium
ABCDEFGH30 kN4 × 3 m3 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

B: 30 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member BG
  13. 13member DG
4.Truss: method of jointsHard
ABCDEFGH30 kN15 kN30 kN4 × 4 m4 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

F: 30 kN →G: 15 kN ↓H: 30 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member BG
  13. 13member DG
5.Shear force & bending momentMedium
w = 2 kN/mABsection2.5 m2.5 m

Find the bending moment Mx at the section x = 2.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mw = 2 kN/m from 0 to 5 mx = 2.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 4 kN/mP = 55 kNABsection1 m3 m

Find the bending moment Mx at the section x = 1 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mP = 55 kN at 1 mw = 4 kN/m from 0 to 4 mx = 1 m
Mx = kN·m
7.Beam deflectionMedium
P = 16 kNABδ1 m4 m

A simply supported beam carries a point load P at a = 1 m from support A. Find the deflection δP under the load.

P = 16 kNa = 1 mL = 5 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δP = mm
8.Beam deflectionHard
w = 4 kN/mAB3 m

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

L = 3 mw = 4 kN/m
RB = kN
9.Column bucklingMedium
PL = 2 md = 25 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 = 2 mE = 70 GPa (aluminium)d = 25 mm
Pcr = kN
10.Column bucklingHard
PL = 2 md = 30 mmcross-section

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

L = 2 mE = 200 GPa (steel)d = 30 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1003030018xdimensions in mm

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

bf = 100 mmtf = 30 mmtw = 18 mmhw = 300 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1801524014xM = 20 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 20 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 180 mmtf = 15 mmtw = 14 mmhw = 240 mmM = 20 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 20.5 kN/m³11 mwater tableXz = 11 m

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

z = 11 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 20.5 kN/m³3 mclayγsat​ = 19 kN/m³5 mwater tableXz = 5.5 m

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

z = 5.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 19 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 170 kPasandclayCc​ = 0.3, Cr​ = 0.06e0​ = 1.05σ′0​ = 105 kPaOCR = 37 mwater table

A 7 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.06 and e₀ = 1.05. At its mid-depth the effective vertical stress is 105 kPa and the overconsolidation ratio is OCR = 3. A new building adds 170 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7 mCc = 0.3Cr = 0.06e0 = 1.05σ′0 = 105 kPaOCR = 3Δσ = 170 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 8 mcv​ = 1.5 m²/year8 msandwater table

A clay layer 8 m thick has a coefficient of consolidation cv = 1.5 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 = 8 mcv = 1.5 m²/yearU = 90%Tv = 0.848double drainage
t = years
17.Hydrostatic forceMedium
gated = 3 mH = 2 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 3 m below the surface. Find the resultant hydrostatic force F on the gate.

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

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

d = 1.5 mH = 3 mb = 1.5 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 75 L/sD = 250 mmL = 400 mf = 0.03

Water flows at 75 L/s through a pipe 400 m long with an inside diameter of 250 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

Q = 75 L/sL = 400 mD = 250 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2Δz = 12 mL = 100 m, D = 200 mm, f = 0.0223× bend (K = 0.3)

Two open reservoirs are joined by a pipe 100 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.022. The water surface of the upper reservoir is 12 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each), a valve (K = 2) 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 = 12 mL = 100 mD = 200 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 2Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 5 my = 1.8 mn = 0.025, S = 0.0008

A rectangular gravel channel is 5 m wide. Water flows uniformly 1.8 m deep. Manning n = 0.025 and the bed slope is S = 0.0008. Find the flow rate Q in m³/s.

b = 5 my = 1.8 mn = 0.025S = 0.0008
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 6 my = 1.5 mn = 0.015, Q = 23 m³/s

A rectangular brickwork channel 6 m wide must carry 23 m³/s in uniform flow at a depth of 1.5 m. Manning n = 0.015. Find the required bed slope S (in m/m).

Q = 23 m³/sb = 6 my = 1.5 mn = 0.015
S = m/m
23.Pumps & pump powerMedium
PQ = 15 L/sH = 36 m

A pump delivers 15 L/s of water (ρ = 1000 kg/m³) against a head of 36 m. The pump efficiency is 85% and the electric motor driving it has an efficiency of 90%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 15 L/sH = 36 mηpump = 85%ηmotor = 90%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 75 L/sΔz = 21 mL = 150 m, D = 200 mm, f = 0.015, ΣK = 8

A pump moves 75 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 21 m higher. The pipe is 150 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 65%. Find the shaft power Pshaft in kW.

Q = 75 L/sΔz = 21 mL = 150 mD = 200 mmf = 0.015ΣK = 8η = 65%
Pshaft = kW
25.Time value of moneyMedium
years0123…8€3 000FV = ?

You invest €3 000 at a nominal rate of 6% per year, compounded monthly. Find the value FV of the investment after 8 years.

PV = €3 0006% / 12n = 8
FV = €
26.Time value of moneyHard
years0123…11€3 000€3 000€3 000FV = ?

You deposit €3 000 at the start of every year for 11 years, the first deposit today. The account pays 4% per year. How much is in the account at the end of year 11? Find FV.

A = €3 000i = 4%n = 11
FV = €
27.NPV & IRRMedium
years0123−60 00017 00023 00013 000

An investment of €60 000 gives these cash flows at the end of years 1 to 3: €17 000, €23 000, €13 000. The cost of capital is 9%. Find the net present value NPV.

r = 9%CF0 = −60 000CF1 = 17 000CF2 = 23 000CF3 = 13 000
NPV = €
28.NPV & IRRHard
years012−40 00022 50021 000

A project costs €40 000 and returns €22 500, €21 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 22 500CF2 = 21 000
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area between −z and z = 0.8740

Drag z so that the shaded area between −z and z under the standard normal curve is 0.8740. Find z to two decimals.

A = 0.8740
z =
30.Normal distributionHard
μ = 178x = ?25%

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

μ = 178σ = 7P = 25%
x = cm

3Solutions

1.Beam support reactions

Answer: RA = 46.88 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​ = 55 kNP2​ = 45 kNABRA​RB​2 m5 m1 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·8 = 55·2 + 45·7
RB = 425/8 = 53.13 kN
ΣFy = 0: RA = 100 − 53.13 = 46.88 kN

Answer

RA = 46.88 kN
2.Beam support reactions

Answer: RB = 29.38 kN

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

w = 2 kN/mP = 55 kNABRA​RB​1 m3 m4 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 2·3 = 6 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·8 = 55·4 + 2·3·2.5
RB = 235/8 = 29.38 kN
ΣFy = 0: RA = 61 − 29.38 = 31.63 kN

Answer

RB = 29.38 kN
3.Truss: method of joints

Answer: member CG

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint C

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

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

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

AB: 22.5 kN (T), BC: 15 kN (T), CD: 15 kN (T), DE: 7.5 kN (T), FG: 22.5 kN (C), GH: 7.5 kN (C), AF: 31.82 kN (C), HE: 10.61 kN (C), BF: 22.5 kN (T), CG: 0, DH: 7.5 kN (T), BG: 10.61 kN (T), DG: 10.61 kN (C)

Answer

Zero-force member: CG
4.Truss: method of joints

Answer: member CG

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint C

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

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

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

AB: 37.5 kN (T), BC: 45 kN (T), CD: 45 kN (T), DE: 37.5 kN (T), FG: 37.5 kN (C), GH: 37.5 kN (C), AF: 10.61 kN (C), HE: 53.03 kN (C), BF: 7.5 kN (T), CG: 0, DH: 7.5 kN (T), BG: 10.61 kN (C), DG: 10.61 kN (C)

Answer

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

Answer: Mx = 6.25 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 = 2·5 = 10 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 2·5·2.5
RB = 25/5 = 5 kN
ΣFy = 0: RA = 10 − 5 = 5 kN
w = 2 kN/mABRA​ = 5RB​ = 5section2.5 m2.5 m

Cut at x = 2.5 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 = 5·2.5 − 2·2.5·1.25 = 6.25 kN·m

Answer

Mx = 6.25 kN·m
6.Shear force & bending moment

Answer: Mx = 47.25 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 = 4·4 = 16 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 55·1 + 4·4·2
RB = 87/4 = 21.75 kN
ΣFy = 0: RA = 71 − 21.75 = 49.25 kN
w = 4 kN/mP = 55 kNABRA​ = 49.25RB​ = 21.75section1 m3 m

Cut at x = 1 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 = 49.25·1 − 4·1·0.5 = 47.25 kN·m

Answer

Mx = 47.25 kN·m
7.Beam deflection

Answer: δP = 7.111 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, a = 1000 mm, b = 4000 mm, L = 5000 mm
EI = 2.4 × 10¹² N·mm²

Deflection under the load

δP = Pa²b²/(3EIL) = 16000·1000²·4000²/(3·2.4 × 10¹²·5000) = 7.111 mm

Answer

δP = 7.111 mm
8.Beam deflection

Answer: RB = 4.5 kN

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition). For a statically indeterminate beam, remove a redundant support and require the deflection there to be zero (compatibility).

Remove the prop

Without the prop the beam is a cantilever. Its free end would deflect under the load.

δload = wL⁴/(8EI)

Compatibility at the prop

The prop force RB alone lifts the free end by RBL³/(3EI). The prop holds B at zero deflection, so the two must cancel. EI cancels out.

RB·L³/(3EI) = wL⁴/(8EI) → RB = 3wL/8 = 3·4·3/8 = 4.5 kN

Answer

RB = 4.5 kN
9.Column buckling

Answer: Pcr = 3.312 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 = 1·2000 = 2000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·19175/2000² = 3312 N = 3.312 kN

Answer

Pcr = 3.312 kN
10.Column buckling

Answer: σcr = 111 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·30⁴/64 = 39761 mm⁴

Radius of gyration and slenderness

A = 706.9 mm²
r = √(I/A) = √(39761/706.9) = 7.5 mm
KL = 0.5·2000 = 1000 mm
KL/r = 1000/7.5 = 133.3

Critical stress

σcr = π²E/(KL/r)² = π²·200000/133.3² = 111 MPa

Answer

σcr = 111 MPa
11.Centroid & second moment of area

Answer: Ix = 93.23 × 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 = 100·30 = 3000 mm², yf = 300 + 30/2 = 315 mm
web: Aw = 18·300 = 5400 mm², yw = 300/2 = 150 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3000·315 + 5400·150)/8400 = 208.9 mm

Parallel-axis theorem

flange: 100·30³/12 + 3000·(315 − 208.9)² = 3.398 × 10⁷ mm⁴
web: 18·300³/12 + 5400·(150 − 208.9)² = 5.925 × 10⁷ mm⁴
Ix = 3.398 × 10⁷ + 5.925 × 10⁷ = 9.323 × 10⁷ mm⁴ = 93.23 × 10⁶ mm⁴

Answer

Ix = 93.23 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σbottom = 87.28 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 = 180·15 = 2700 mm², yf = 240 + 15/2 = 247.5 mm
web: Aw = 14·240 = 3360 mm², yw = 240/2 = 120 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2700·247.5 + 3360·120)/6060 = 176.8 mm

Parallel-axis theorem

flange: 180·15³/12 + 2700·(247.5 − 176.8)² = 1.354 × 10⁷ mm⁴
web: 14·240³/12 + 3360·(120 − 176.8)² = 2.697 × 10⁷ mm⁴
Ix = 1.354 × 10⁷ + 2.697 × 10⁷ = 4.051 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 176.8 mm
σ = M·y/I = 2 × 10⁷·176.8/4.051 × 10⁷ = 87.28 MPa

Answer

σbottom = 87.28 MPa
13.Effective stress in soil

Answer: σ′ = 130.5 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·zw + γsat·(z − zw) = 15·3 + 20.5·8 = 209 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·8 = 78.48 kPa

Effective stress

σ′ = σ − u = 209 − 78.48 = 130.5 kPa

Answer

σ′ = 130.5 kPa
14.Effective stress in soil

Answer: σ′ = 59.35 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·1 + γsat,sand·2 + γsat,clay·2.5
σ = 15·1 + 20.5·2 + 19·2.5 = 103.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·4.5 = 44.15 kPa

Effective stress

σ′ = σ − u = 103.5 − 44.15 = 59.35 kPa

Answer

σ′ = 59.35 kPa
15.Consolidation settlement

Answer: S = 85.67 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 = 3·105 = 315 kPa

Compare with the preconsolidation pressure

σ′f = 105 + 170 = 275 kPa ≤ 315 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.06·7/(1 + 1.05)·log₁₀(275/105) = 85.67 mm

Answer

S = 85.67 mm
16.Consolidation settlement

Answer: t = 9.045 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 = 8/2 = 4 m

Time

t = Tv·Hdr²/cv = 0.848·4²/1.5 = 9.045 years

Answer

t = 9.045 years
17.Hydrostatic force

Answer: F = 117.7 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 = 3 + 2/2 = 4 m
A = H·b = 2·1.5 = 3 m²
gated = 3 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·4·3 = 117.7 kN

Answer

F = 117.7 kN
18.Hydrostatic force

Answer: F = 135.7 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 = 1.5 + 3/2 = 3 m
A = H·b = 3·1.5 = 4.5 m²
gated = 1.5 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·3·4.5 = 135.7 kN

Answer

F = 135.7 kN
19.Pipe friction & head loss

Answer: hf = 5.711 m

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

Mean velocity

A = π·0.25²/4 = 0.04909 m²
V = Q/A = 0.075/0.04909 = 1.528 m/s

Velocity head

V²/(2g) = 1.528²/(2·9.81) = 0.119 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(400/0.25)·1.528²/(2·9.81) = 5.711 m

Answer

hf = 5.711 m
20.Pipe friction & head loss

Answer: Q = 122.8 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 = 0.022·100/0.2 = 11
ΣK = 0.5 + 3·0.3 + 2 + 1.0 = 4.4

Energy equation

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

12 = (11 + 4.4)·V²/(2·9.81)
V = √(2·9.81·12/15.4) = 3.91 m/s

Flow rate

Q = V·π·D²/4 = 3.91·0.03142 = 0.1228 m³/s = 122.8 L/s

Answer

Q = 122.8 L/s
21.Open-channel flow (Manning)

Answer: Q = 10.5 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 = 5·1.8 = 9 m²
P = b + 2y = 5 + 2·1.8 = 8.6 m
R = A/P = 1.047 m

Velocity

V = (1/0.025)·1.0472/3·0.00081/2 = 1.166 m/s

Flow rate

Q = A·V = 9·1.166 = 10.5 m³/s

Answer

Q = 10.5 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.001469 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 = 6·1.5 = 9 m²
P = b + 2y = 6 + 2·1.5 = 9 m
R = A/P = 1 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.015·23/(9·1) = 0.03833
S = 0.03833² = 0.001469

Answer

S = 0.001469

That is a fall of 1.469 m per kilometre.

23.Pumps & pump power

Answer: Pel = 6.925 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 = 1000·9.81·0.015·36 = 5.297 kW

Shaft power

Pshaft = 5.297/0.85 = 6.232 kW

Electrical power

Pel = 6.232/0.9 = 6.925 kW

Answer

Pel = 6.925 kW
24.Pumps & pump power

Answer: Pshaft = 30.1 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 = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (11.25 + 8)·0.2905 = 5.592 m

Pump head

H = Δz + hL = 21 + 5.592 = 26.59 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.075·26.59/0.65 = 30.1 kW

Answer

Pshaft = 30.1 kW
25.Time value of money

Answer: FV = 4842 €

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 = 0.06/12 = 0.005
N = m·n = 12·8 = 96

Future value

FV = 3 000·(1 + 0.005)96 = 3 000·1.614 = €4 842.43

Answer

FV = €4 842.43
26.Time value of money

Answer: FV = 42077 €

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)11 − 1)/0.04 = 13.49

Annuity due

Each deposit is invested one year longer.

FV = 3 000·13.49·1.04 = €42 077.42

Answer

FV = €42 077.42
27.NPV & IRR

Answer: NPV = −15007 €

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 + 0.09)1 = 17 000/1.09 = 15 596.33
CF2/(1 + 0.09)2 = 23 000/1.188 = 19 358.64
CF3/(1 + 0.09)3 = 13 000/1.295 = 10 038.39

Add them up

NPV = €−15 006.64

Answer

NPV = €−15 006.64

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

28.NPV & IRR

Answer: IRR = 5.849 %

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(5%) = 476.19
NPV(10%) = −2 190.08

Narrow down

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

IRR ≈ 5 + 5·476.19/(476.19 − (−2 190.08)) = 5.893%
exact: NPV(5.849%) = 0 → IRR = 5.849%

Answer

IRR = 5.849%
29.Normal distribution

Answer: z = 1.53

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 + 0.8740)/2 = 0.9370

Read the z-table backwards

Find 0.9370 inside the table and read off z.

z = 1.53

Answer

z = 1.53
30.Normal distribution

Answer: x = 173.3 cm

Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.

z for the percentile

Φ(z) = 0.25 → z = −0.6745

Back to x

x = 178 + −0.6745·7 = 173.28 cm

Answer

x = 173.28 cm

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