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​ = 8 kN/mP = 30 kNABRA​ = ?1 m7 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that rises from zero at A to 8 kN/m at B. A point load P also acts at 1 m from A. Find the vertical support reaction RA.

L = 8 mw0 = 8 kN/mP = 30 kN at 1 m
RA = kN
2.Beam support reactionsHard
w = 8 kN/mP = 25 kNABRA​RB​ = ?1 m2 m1 m1 m

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

L = 5 mP = 25 kN at 4 mw = 8 kN/m from 1 to 3 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB20 kN4 m1 m2 m

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

span = 4 mheight = 2 mB is 1 m from Avertical load = 20 kN
FAB = kN
4.Truss: method of jointsHard
ABCDEFGH35 kN15 kN25 kN20 kN15 kN4 × 4 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: 35 kN ↓D: 15 kN ↓F: 25 kN ↓H: 20 kN ↓H: 15 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
P1​ = 35 kNP2​ = 35 kNABC1 m7 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. It carries a point load P1 between the supports and a point load P2 at C. Find the shear force Vx just to the left of support B. Use sagging moments positive and upward shear on the left face positive.

L = 9 mP1 = 35 kN at 1 mP2 = 35 kN at 9 msupports at x = 0 and x = 8 m
Vx = kN
6.Shear force & bending momentHard
w = 3 kN/mP = 20 kNABsection3 m1 m

Find the bending moment Mx at the section x = 3 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mP = 20 kN at 3 mw = 3 kN/m from 0 to 4 mx = 3 m
Mx = kN·m
7.Beam deflectionMedium
w = 5 kN/mδL = 5 m

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

w = 5 kN/mL = 5 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 6 kN/mδL = 4 m

A simply supported beam carries a uniformly distributed load w. Its deflection may not exceed span/360. Find the smallest second moment of area Ireq that meets this limit.

w = 6 kN/mL = 4 mE = 200 GPa (steel)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 1 md = 20 mmcross-section

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

L = 1 mE = 200 GPa (steel)d = 20 mm
Pcr = kN
10.Column bucklingHard
P = 150 kNL = 2 md = ?cross-section

A solid round column of length L made of steel is pinned at both ends. It must carry 150 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 150 kNn = 3L = 2 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
2802022020xdimensions 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 = 20 mmhw = 220 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1801524014xsagging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 40 MPa in tension and 100 MPa in compression. Find the largest sagging bending moment Mallow the beam can carry.

bf = 180 mmtf = 15 mmtw = 14 mmhw = 240 mmσt,allow = 40 MPaσc,allow = 100 MPa
Mallow = kN·m
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 19.5 kN/m³12 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 = 15 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 17 kN/m³γsat​ = 19.5 kN/m³3 mclayγsat​ = 18.5 kN/m³6 mwater tableXz = 6 m

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

z = 6 mzw = 1 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 19.5 kN/m³clay: γsat = 18.5 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 85 kPasandclayCc​ = 0.3, Cr​ = 0.05e0​ = 0.6σ′0​ = 85 kPaσ′p​ = 205 kPa5.5 mwater table

A 5.5 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.05 and e₀ = 0.6. At its mid-depth the effective vertical stress is 85 kPa and the preconsolidation pressure is 205 kPa. A new building adds 85 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 5.5 mCc = 0.3Cr = 0.05e0 = 0.6σ′0 = 85 kPaσ′p = 205 kPaΔσ = 85 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 8.5 mcv​ = 2.5 m²/year8.5 mimpervious rockwater table

A clay layer 8.5 m thick has a coefficient of consolidation cv = 2.5 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 60% average consolidation the time factor is Tv = 0.287. How many years t does the layer take to reach 60% consolidation?

H = 8.5 mcv = 2.5 m²/yearU = 60%Tv = 0.287single drainage
t = years
17.Hydrostatic forceMedium
gated = 3 mH = 2.5 m

A vertical rectangular gate 1 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 = 2.5 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2.5 mH = 1 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 2.5 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 2.5 mH = 1 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
Q = 150 L/sD = 250 mmL = 200 mf = 0.03

Water flows at 150 L/s through a pipe 200 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 = 150 L/sL = 200 mD = 250 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 0.2Δz = ?L = 300 m, D = 300 mm, f = 0.023× bend (K = 0.3)

Two open reservoirs are joined by a pipe 300 m long with an inside diameter of 300 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 = 0.2) 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 100 L/s?

Q = 100 L/sL = 300 mD = 300 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 0.2Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
D = 300 mmn = 0.013, S = 0.002

A concrete storm sewer with an inside diameter of 300 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 = 300 mmn = 0.013S = 0.002
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2 my = 0.8 m3 : 1n = 0.015, Q = 6.6 m³/s

A trapezoidal brickwork channel with a bottom width of 2 m and side slopes of 3:1 (horizontal:vertical) must carry 6.6 m³/s in uniform flow at a depth of 0.8 m. Manning n = 0.015. Find the required bed slope S (in m/m).

Q = 6.6 m³/sb = 2 my = 0.8 mz = 3n = 0.015
S = m/m
23.Pumps & pump powerMedium
PQ = 20 L/sH = 28 m

A pump delivers 20 L/s of water (ρ = 1000 kg/m³) against a head of 28 m. The pump efficiency is 70% and the electric motor driving it has an efficiency of 92%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 20 L/sH = 28 mηpump = 70%ηmotor = 92%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 40 L/sΔz = 19 mL = 100 m, D = 150 mm, f = 0.025, ΣK = 5

A pump moves 40 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 19 m higher. The pipe is 100 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 5 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 65%. Find the shaft power Pshaft in kW.

Q = 40 L/sΔz = 19 mL = 100 mD = 150 mmf = 0.025ΣK = 5η = 65%
Pshaft = kW
25.Time value of moneyMedium
years0123…9PV = ?€15 000

You need €15 000 in 9 years. An account pays 4.8% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €15 0004.8% / 4n = 9
PV = €
26.Time value of moneyHard
months0123…240€200€200€200FV = ?

You save €200 at the end of every month for 20 years. The account pays 4.8% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €2004.8% / 12N = 240
FV = €
27.NPV & IRRMedium
years0123−60 00022 00022 00017 000

An investment of €60 000 gives these cash flows at the end of years 1 to 3: €22 000, €22 000, €17 000. The cost of capital is 15%. Find the net present value NPV.

r = 15%CF0 = −60 000CF1 = 22 000CF2 = 22 000CF3 = 17 000
NPV = €
28.NPV & IRRHard
years0123456−50 0008 500+3%+3%+3%+3%+3%r = 12%, NPV = ?

A project costs €50 000 today. Its cash flow is €8 500 at the end of year 1 and grows by 3% per year until the last cash flow at the end of year 6. The cost of capital is 12%. Find the net present value NPV.

C0 = €50 000CF1 = €8 500g = 3%n = 6r = 12%
NPV = €
29.Normal distributionMedium
120 kg125.1 kgT = X₁ + … + X₁₀?

The masses of boxes are independent and normal with mean 12 kg and standard deviation 0.8 kg. Find the probability P that the total mass of 10 of them exceeds 125.1 kg. Round z to two decimals.

μ = 12 kgσ = 0.8 kgn = 10> 125.1 kg
P =
30.Normal distributionHard
10 g0X − Y?

The mass X of a product from line 1 and Y from line 2 are independent and normal: X has mean 500 g and standard deviation 8 g, Y has mean 490 g and standard deviation 6 g. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 500 g, σX = 8 gμY = 490 g, σY = 6 g
P =

3Solutions

1.Beam support reactions

Answer: RA = 36.92 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 = ½·8·8 = 32 kN
x̄ = 2L/3 = 5.333 m

Equilibrium

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

ΣMA = 0: RB·8 = 32·5.333 + 30·1
RB = 25.08 kN
RA = 62 − 25.08 = 36.92 kN

Answer

RA = 36.92 kN
2.Beam support reactions

Answer: RB = 26.4 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 = 8 kN/mP = 25 kNABRA​RB​1 m2 m1 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.

UDL resultant: W = w·ℓ = 8·2 = 16 kN, acting at x̄ = 2 m
ΣMA = 0: RB·5 = 25·4 + 8·2·2
RB = 132/5 = 26.4 kN
ΣFy = 0: RA = 41 − 26.4 = 14.6 kN

Answer

RB = 26.4 kN
3.Truss: method of joints

Answer: FAB = −16.77 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·4 = 20·1 → Cy = 5 kN
ΣFy = 0: Ay = 20 − 5 = 15 kN

Joint A

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

sin α = 2/2.236 = 0.8944
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −15/0.8944 = −16.77 kN

Answer

FAB = −16.77 kN (compression)
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: 60.42 kN (T), BC: 55.83 kN (T), CD: 55.83 kN (T), DE: 51.25 kN (T), FG: 75.42 kN (C), GH: 66.25 kN (C), AF: 94.27 kN (C), HE: 64.06 kN (C), BF: 31.56 kN (T), CG: 0, DH: 18.44 kN (T), BG: 5.729 kN (T), DG: 5.729 kN (C)

Answer

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

Answer: Vx = −8.75 kN

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

Support reactions

Equilibrium of the whole beam. The overhang load also acts about A.

ΣMA = 0: RB·8 = 35·1 + 35·9
RB = 350/8 = 43.75 kN
ΣFy = 0: RA = 70 − 43.75 = 26.25 kN

Cut just left of B and keep the left part

Vx = RA − P1 = 26.25 − 35 = −8.75 kN

Answer

Vx = −8.75 kN
6.Shear force & bending moment

Answer: Mx = 19.5 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 = 3·4 = 12 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 20·3 + 3·4·2
RB = 84/4 = 21 kN
ΣFy = 0: RA = 32 − 21 = 11 kN
w = 3 kN/mP = 20 kNABRA​ = 11RB​ = 21section3 m1 m

Cut at x = 3 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 = 11·3 − 3·3·1.5 = 19.5 kN·m

Answer

Mx = 19.5 kN·m
7.Beam deflection

Answer: δmax = 16.95 mm

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

Consistent units

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

w = 5 N/mm, L = 5000 mm
EI = 2.4 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·5·5000⁴/(384·2.4 × 10¹²) = 16.95 mm

Answer

δmax = 16.95 mm
8.Beam deflection

Answer: Ireq = 9 × 10⁶ mm⁴

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).

Deflection limit

δallow = L/360 = 4000/360 = 11.11 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·6·4000⁴/(384·200000·11.11) = 9 × 10⁶ mm⁴
Ireq = 9 × 10⁶ mm⁴

Answer

Ireq = 9 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 31.64 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·20⁴/64 = 7854 mm⁴

Effective length

KL = 0.7·1000 = 700 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·7854/700² = 31639 N = 31.64 kN

Answer

Pcr = 31.64 kN
10.Column buckling

Answer: d = 65.65 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 = 3·150000 = 450000 N
KL = 1·2000 = 2000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·450000·2000²/(π³·200000))^(1/4) = 65.65 mm

Answer

d = 65.65 mm

Check: the slenderness KL/r is 121.9, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 53.41 × 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 = 220 + 20/2 = 230 mm
web: Aw = 20·220 = 4400 mm², yw = 220/2 = 110 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (5600·230 + 4400·110)/10000 = 177.2 mm

Parallel-axis theorem

flange: 280·20³/12 + 5600·(230 − 177.2)² = 1.58 × 10⁷ mm⁴
web: 20·220³/12 + 4400·(110 − 177.2)² = 3.762 × 10⁷ mm⁴
Ix = 1.58 × 10⁷ + 3.762 × 10⁷ = 5.341 × 10⁷ mm⁴ = 53.41 × 10⁶ mm⁴

Answer

Ix = 53.41 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 9.166 kN·m

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.

Centroid

ȳ = (2700·247.5 + 3360·120)/6060 = 176.8 mm
top edge: c = 255 − 176.8 = 78.19 mm

Second moment of area

I = 180·15³/12 + 2700·70.69² + 14·240³/12 + 3360·56.81² = 4.051 × 10⁷ mm⁴

Moment allowed by each edge

Sagging: the top is in compression, the bottom in tension.

top edge: M = 100·4.051 × 10⁷/78.19 = 51.81 kN·m
bottom edge: M = 40·4.051 × 10⁷/176.8 = 9.166 kN·m

Governing value

Mallow = min = 9.166 kN·m (bottom edge)

Answer

Mallow = 9.166 kN·m
13.Effective stress in soil

Answer: σ′ = 63.45 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) = 15·1 + 19.5·5 = 112.5 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 = 112.5 − 49.05 = 63.45 kPa

Answer

σ′ = 63.45 kPa
14.Effective stress in soil

Answer: σ = 111.5 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·1 + γsat,sand·2 + γsat,clay·3
σ = 17·1 + 19.5·2 + 18.5·3 = 111.5 kPa

Answer

σ = 111.5 kPa
15.Consolidation settlement

Answer: S = 51.74 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 = 85 + 85 = 170 kPa ≤ 205 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·5.5/(1 + 0.6)·log₁₀(170/85) = 51.74 mm

Answer

S = 51.74 mm
16.Consolidation settlement

Answer: t = 8.294 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 = 8.5 m

Time

t = Tv·Hdr²/cv = 0.287·8.5²/2.5 = 8.294 years

Answer

t = 8.294 years
17.Hydrostatic force

Answer: F = 104.2 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 + 2.5/2 = 4.25 m
A = H·b = 2.5·1 = 2.5 m²
gated = 3 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·4.25·2.5 = 104.2 kN

Answer

F = 104.2 kN
18.Hydrostatic force

Answer: ycp = 3.028 m

Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.

Centroid depth and area

yc = d + H/2 = 2.5 + 1/2 = 3 m
A = H·b = 1·1.5 = 1.5 m²
gated = 2.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3·1.5 = 44.15 kN

Centre of pressure

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

Ic = b·H³/12 = 1.5·1³/12 = 0.125 m⁴
ycp = yc + Ic/(yc·A) = 3 + 0.125/(3·1.5) = 3.028 m

Answer

ycp = 3.028 m
19.Pipe friction & head loss

Answer: hf = 11.42 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 = 0.15/0.04909 = 3.056 m/s

Velocity head

V²/(2g) = 3.056²/(2·9.81) = 0.4759 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(200/0.25)·3.056²/(2·9.81) = 11.42 m

Answer

hf = 11.42 m
20.Pipe friction & head loss

Answer: Δz = 2.305 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 = 0.1/0.07069 = 1.415 m/s
V²/(2g) = 0.102 m

Loss coefficients

f·L/D = 0.02·300/0.3 = 20
ΣK = 0.5 + 3·0.3 + 0.2 + 1.0 = 2.6

Total head loss

hf = 20·0.102 = 2.04 m
hm = 2.6·0.102 = 0.2652 m
Δz = hf + hm = 2.305 m

Answer

Δz = 2.305 m
21.Open-channel flow (Manning)

Answer: Q = 0.04325 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 = 0.07069 m², R = D/4 = 0.075 m

Velocity

V = (1/0.013)·0.0752/3·0.0021/2 = 0.6118 m/s

Flow rate

Q = A·V = 0.07069·0.6118 = 0.04325 m³/s

Answer

Q = 0.04325 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002001 m/m

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

Geometry

A = (b + z·y)·y = (2 + 3·0.8)·0.8 = 3.52 m²
P = b + 2y·√(1 + z²) = 2 + 2·0.8·√(1 + 3²) = 7.06 m
R = A/P = 0.4986 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.015·6.6/(3.52·0.6288) = 0.04473
S = 0.04473² = 0.002001

Answer

S = 0.002001

That is a fall of 2.001 m per kilometre.

23.Pumps & pump power

Answer: Pel = 8.53 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 = 1000·9.81·0.02·28 = 5.494 kW

Shaft power

Pshaft = 5.494/0.7 = 7.848 kW

Electrical power

Pel = 7.848/0.92 = 8.53 kW

Answer

Pel = 8.53 kW
24.Pumps & pump power

Answer: Pshaft = 14.89 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 = 0.04/0.01767 = 2.264 m/s
V²/(2g) = 0.2611 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (16.67 + 5)·0.2611 = 5.658 m

Pump head

H = Δz + hL = 19 + 5.658 = 24.66 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.04·24.66/0.65 = 14.89 kW

Answer

Pshaft = 14.89 kW
25.Time value of money

Answer: PV = 9763 €

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 = 0.048/4 = 0.012
N = 4·9 = 36

Present value

PV = FV/(1 + i)N = 15 000/1.536 = €9 763.21

Answer

PV = €9 763.21
26.Time value of money

Answer: FV = 80335 €

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

Monthly rate and number of deposits

i = 0.048/12 = 0.004
N = 12·20 = 240

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 200·(2.607 − 1)/0.004 = €80 335.01

Answer

FV = €80 335.01

You paid in €48 000 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −13057 €

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 + 0.15)1 = 22 000/1.15 = 19 130.43
CF2/(1 + 0.15)2 = 22 000/1.322 = 16 635.16
CF3/(1 + 0.15)3 = 17 000/1.521 = 11 177.78

Add them up

NPV = €−13 056.63

Answer

NPV = €−13 056.63

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

28.NPV & IRR

Answer: NPV = −12689 €

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 the growing annuity

((1.03)/(1.12))6 = 0.6049
PV = 8 500/(0.12 − 0.03)·(1 − 0.6049) = 37 310.84

NPV

NPV = 37 310.84 − 50 000 = −€12 689.16

Answer

NPV = −€12 689.16

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

29.Normal distribution

Answer: P = 0.02169

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 total

μT = 120 kg, σT = 0.8·√10 = 2.53 kg

Standardise

z = (125.1 − 120)/2.53 = 2.02

Probability

P = 1 − Φ(2.02) = 0.02169

Answer

P = 0.02169
30.Normal distribution

Answer: P = 0.8413

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 = 500 − 490 = 10 g, σ = 10 g

Standardise

z = (0 − 10)/10 = −1

Probability

P = 1 − Φ(−1) = 0.8413

Answer

P = 0.8413

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