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​ = 35 kNP2​ = 75 kNABCRB​ = ?0.5 m2.5 m2 m

The beam has a pin at A and a roller at B, 3 m from A, and overhangs B to the free end C. Find the vertical reaction RB, taking upward as positive.

AB = 3 mAC = 5 mP1 = 35 kN at 0.5 mP2 = 75 kN at 5 m
RB = kN
2.Beam support reactionsHard
w = 8 kN/mP = 15 kNABRA​RB​ = ?1 m2 m1 m

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

L = 4 mP = 15 kN at 3 mw = 8 kN/m from 0 to 1 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB40 kN4 m1 m4 m

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

span = 4 mheight = 4 mB is 1 m from Avertical load = 40 kN
FAC = kN
4.Truss: method of jointsHard
ABCDEFGH15 kN20 kN20 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: 15 kN ↓D: 20 kN ↓F: 20 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​ = 55 kNP2​ = 80 kNABC2.5 m1.5 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 bending moment Mx under the load P1. Use sagging moments positive and upward shear on the left face positive.

L = 5 mP1 = 55 kN at 2.5 mP2 = 80 kN at 5 msupports at x = 0 and x = 4 m
Mx = kN·m
6.Shear force & bending momentHard
w = 8 kN/mAB1 m2 m1 m

The simply supported beam carries a uniformly distributed load over part of its span. Find the maximum bending moment Mmax in the beam.

L = 4 mw = 8 kN/m from 1 to 3 m
Mmax = kN·m
7.Beam deflectionMedium
P = 23 kNABδ1 m3 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 = 23 kNa = 1 mL = 4 mE = 70 GPa (aluminium)I = 36 × 10⁶ mm⁴
δP = mm
8.Beam deflectionHard
w = 4 kN/mABδ3.5 m

A simply supported timber beam of rectangular section, 75 mm wide, carries a uniformly distributed load w over its whole span. Its midspan deflection may not exceed span/250. Find the smallest depth hreq of the section.

w = 4 kN/mL = 3.5 mE = 11 GPa (timber)b = 75 mm
hreq = mm
9.Column bucklingMedium
PL = 6 m30 × 100 mmcross-section

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

L = 6 mE = 200 GPa (steel)b × h = 30 × 100 mm
Pcr = kN
10.Column bucklingHard
P = 85 kNL = 4 md = ?cross-section

A solid round column of length L made of steel is pinned at both ends. It must carry 85 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 85 kNn = 2.5L = 4 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
xD = 100d = 76dimensions in mm

A circular tube has outside diameter D = 100 mm and inside diameter d = 76 mm. Find its radius of gyration r about the horizontal centroidal axis.

D = 100 mmd = 76 mm
r = mm
12.Centroid & second moment of areaHard
2802518020xM = 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 = 280 mmtf = 25 mmtw = 20 mmhw = 180 mmM = 20 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 19.5 kN/m³13 mwater tableXz = 7 m

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

z = 7 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 19.5 kN/m³5 mclayγsat​ = 18.5 kN/m³6 mwater tableXz = 8 m

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

z = 8 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 19.5 kN/m³clay: γsat = 18.5 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 15 kPasandclayCc​ = 0.3, Cr​ = 0.06e0​ = 0.7σ′0​ = 45 kPaσ′p​ = 75 kPa2.5 mwater table

A 2.5 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.06 and e₀ = 0.7. At its mid-depth the effective vertical stress is 45 kPa and the preconsolidation pressure is 75 kPa. A new building adds 15 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2.5 mCc = 0.3Cr = 0.06e0 = 0.7σ′0 = 45 kPaσ′p = 75 kPaΔσ = 15 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 5 mcv​ = 5 m²/year5 mimpervious rockwater table

A clay layer 5 m thick has a coefficient of consolidation cv = 5 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 80% average consolidation the time factor is Tv = 0.567. How many years t does the layer take to reach 80% consolidation?

H = 5 mcv = 5 m²/yearU = 80%Tv = 0.567single drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 2.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 2.5 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 0.5 mH = 1 m

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

d = 0.5 mH = 1 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 60 L/sD = 200 mmL = 50 mf = 0.028

Water flows at 60 L/s through a pipe 50 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.028 and g = 9.81 m/s². Find the friction head loss hf.

Q = 60 L/sL = 50 mD = 200 mmf = 0.028g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10free outletH = ?L = 400 m, D = 200 mm, f = 0.0153× bend (K = 0.3)

A pipe 400 m long with an inside diameter of 200 mm (Darcy friction factor f = 0.015) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each) and a valve (K = 10). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 40 L/s?

Q = 40 L/sL = 400 mD = 200 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 10
H = m
21.Open-channel flow (Manning)Medium
b = 5 my = 0.5 m3 : 1n = 0.025, S = 0.0008

A trapezoidal gravel channel has a bottom width of 5 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 0.5 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 = 0.5 mz = 3n = 0.025S = 0.0008
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2.5 my = 1.9 mn = 0.014, Q = 15 m³/s

A rectangular unfinished concrete channel 2.5 m wide must carry 15 m³/s in uniform flow at a depth of 1.9 m. Manning n = 0.014. Find the required bed slope S (in m/m).

Q = 15 m³/sb = 2.5 my = 1.9 mn = 0.014
S = m/m
23.Pumps & pump powerMedium
PQ = 30 L/sH = 66 m

A pump with an efficiency of 75% delivers 30 L/s of water (ρ = 1000 kg/m³) against a head of 66 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 30 L/sH = 66 mη = 75%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 80 L/sΔz = 9 mL = 300 m, D = 200 mm, f = 0.02, ΣK = 6

A pump moves 80 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 9 m higher. The pipe is 300 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 80 L/sΔz = 9 mL = 300 mD = 200 mmf = 0.02ΣK = 6
H = m
25.Time value of moneyMedium
years0123…8PV = ?€3 000€3 000€3 000€3 000

An annuity pays €3 000 at the end of each year for 8 years. The interest rate is 7% per year. Find the present value PV of the annuity.

A = €3 000i = 7%n = 8
PV = €
26.Time value of moneyHard
months0123…36€12 000A?AAA

A loan of €12 000 is repaid with equal monthly payments over 3 years. The interest rate is 7.2% per year, compounded monthly. Find the monthly payment A.

P = €12 0007.2% / 12N = 36
A = €
27.NPV & IRRMedium
years0123…9−100 00010 000+1%+1%…r = 10%, NPV = ?

A project costs €100 000 today. It generates €10 000 at the end of the first year, and the cash flow then grows by 1% per year forever. The cost of capital is 10%. Find the net present value NPV.

C0 = €100 000CF1 = €10 000g = 1%r = 10%
NPV = €
28.NPV & IRRHard
years0123−25 00013 00011 00013 500

A project costs €25 000 and returns €13 000, €11 000, €13 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −25 000CF1 = 13 000CF2 = 11 000CF3 = 13 500
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area between −z and z = 0.5587

Drag z so that the shaded area between −z and z under the standard normal curve is 0.5587. Find z to two decimals.

A = 0.5587
z =
30.Normal distributionHard
235240245250255260265gtop 25%

The bag weights are normally distributed with mean 250 g and standard deviation 5 g. Drag the cut-off so the shaded top 25% is to the right of it. Find the cut-off x.

μ = 250 gσ = 5 g25%
x = g

3Solutions

1.Beam support reactions

Answer: RB = 130.8 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.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·3 = 35·0.5 + 75·5
RB = 392.5/3 = 130.8 kN

Vertical equilibrium

RA = 35 + 75 − 130.8 = −20.83 kN

Answer

RB = 130.8 kN

RA is negative: the pin at A has to hold the beam down.

2.Beam support reactions

Answer: RB = 12.25 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 = 15 kNABRA​RB​1 m2 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 = 8·1 = 8 kN, acting at x̄ = 0.5 m
ΣMA = 0: RB·4 = 15·3 + 8·1·0.5
RB = 49/4 = 12.25 kN
ΣFy = 0: RA = 23 − 12.25 = 10.75 kN

Answer

RB = 12.25 kN
3.Truss: method of joints

Answer: FAC = 7.5 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.

ABBCACACB40 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·4 = 40·1 → Cy = 10 kN
ΣFy = 0: Ay = 40 − 10 = 30 kN

Joint C

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

sin γ = 4/5 = 0.8, cos γ = 3/5 = 0.6
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −10/0.8 = −12.5 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−12.5)·0.6 = 7.5 kN

Answer

FAC = 7.5 kN (tension)
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: 31.25 kN (T), BC: 27.5 kN (T), CD: 27.5 kN (T), DE: 23.75 kN (T), FG: 31.25 kN (C), GH: 23.75 kN (C), AF: 15.91 kN (C), HE: 33.59 kN (C), BF: 11.25 kN (T), CG: 0, DH: 23.75 kN (T), BG: 5.303 kN (T), DG: 5.303 kN (C)

Answer

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

Answer: Mx = 1.563 kN·m

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

Support reactions

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

ΣMA = 0: RB·4 = 55·2.5 + 80·5
RB = 537.5/4 = 134.4 kN
ΣFy = 0: RA = 135 − 134.4 = 0.625 kN

Cut under P1 and keep the left part

Mx = RA·2.5 = 0.625·2.5 = 1.563 kN·m

Answer

Mx = 1.563 kN·m
6.Shear force & bending moment

Answer: Mmax = 12 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.

UDL resultant: W = w·ℓ = 8·2 = 16 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 8·2·2
RB = 32/4 = 8 kN
ΣFy = 0: RA = 16 − 8 = 8 kN

Zero shear

The shear force starts at RA, stays constant over any unloaded part and falls with slope w inside the load.

RA − w·(x0 − 1) = 0
x0 = 1 + 8/8 = 2 m

Maximum moment

Mmax = RA·x0 − w·(x0 − 1)²/2 = 8·2 − 8·1²/2 = 12 kN·m

Answer

Mmax = 12 kN·m
7.Beam deflection

Answer: δP = 6.845 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 = 23000 N, a = 1000 mm, b = 3000 mm, L = 4000 mm
EI = 2.52 × 10¹² N·mm²

Deflection under the load

δP = Pa²b²/(3EIL) = 23000·1000²·3000²/(3·2.52 × 10¹²·4000) = 6.845 mm

Answer

δP = 6.845 mm
8.Beam deflection

Answer: hreq = 201 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 = 4 N/mm, L = 3500 mm, E = 11000 N/mm²

Deflection limit

δallow = L/250 = 3500/250 = 14 mm

Required second moment of area

Ireq = 5wL⁴/(384·E·δallow) = 5·4·3500⁴/(384·11000·14) = 5.075 × 10⁷ mm⁴

Required depth

bh³/12 = Ireq → h = (12·5.075 × 10⁷/75)1/3 = 201 mm

Answer

hreq = 201 mm

In practice, choose the next standard depth above this value.

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 = 1·6000 = 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: d = 76.97 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 = 2.5·85000 = 212500 N
KL = 1·4000 = 4000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·212500·4000²/(π³·200000))^(1/4) = 76.97 mm

Answer

d = 76.97 mm

Check: the slenderness KL/r is 207.9, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: r = 31.4 mm

Second moment of area: for a rectangle about its own centroidal axis I = bh³/12, and about its base bh³/3 (parallel-axis theorem I = Ic + A·d²). A hole is handled by subtracting its I, as long as both parts share the same axis. The elastic section modulus is S = I/c, where c is the distance to the extreme fibre. The radius of gyration r = √(I/A) is the distance at which the whole area would give the same I; it is used in column buckling.

Net area and second moment of area

A = π(D² − d²)/4 = 3318 mm²
I = π(D⁴ − d⁴)/64 = 3.271 × 10⁶ mm⁴

Radius of gyration

r = √(I/A) = √(3.271 × 10⁶/3318) = 31.4 mm

Answer

r = 31.4 mm
12.Centroid & second moment of area

Answer: σbottom = 89.95 MPa

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

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 280·25 = 7000 mm², yf = 180 + 25/2 = 192.5 mm
web: Aw = 20·180 = 3600 mm², yw = 180/2 = 90 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (7000·192.5 + 3600·90)/10600 = 157.7 mm

Parallel-axis theorem

flange: 280·25³/12 + 7000·(192.5 − 157.7)² = 8.847 × 10⁶ mm⁴
web: 20·180³/12 + 3600·(90 − 157.7)² = 2.621 × 10⁷ mm⁴
Ix = 8.847 × 10⁶ + 2.621 × 10⁷ = 3.506 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 157.7 mm
σ = M·y/I = 2 × 10⁷·157.7/3.506 × 10⁷ = 89.95 MPa

Answer

σbottom = 89.95 MPa
13.Effective stress in soil

Answer: σ′ = 85.26 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) = 15.5·3 + 19.5·4 = 124.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·4 = 39.24 kPa

Effective stress

σ′ = σ − u = 124.5 − 39.24 = 85.26 kPa

Answer

σ′ = 85.26 kPa
14.Effective stress in soil

Answer: σ = 141 kPa

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

Total stress

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

σ = γd·3 + γsat,sand·2 + γsat,clay·3
σ = 15.5·3 + 19.5·2 + 18.5·3 = 141 kPa

Answer

σ = 141 kPa
15.Consolidation settlement

Answer: S = 11.02 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 = 45 + 15 = 60 kPa ≤ 75 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.06·2.5/(1 + 0.7)·log₁₀(60/45) = 11.02 mm

Answer

S = 11.02 mm
16.Consolidation settlement

Answer: t = 2.835 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 = 5 m

Time

t = Tv·Hdr²/cv = 0.567·5²/5 = 2.835 years

Answer

t = 2.835 years
17.Hydrostatic force

Answer: F = 159.4 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 = 2 + 2.5/2 = 3.25 m
A = H·b = 2.5·2 = 5 m²
gated = 2 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.25·5 = 159.4 kN

Answer

F = 159.4 kN
18.Hydrostatic force

Answer: F = 14.71 kN

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

Centroid depth and area

yc = d + H/2 = 0.5 + 1/2 = 1 m
A = H·b = 1·1.5 = 1.5 m²
gated = 0.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·1·1.5 = 14.71 kN

Answer

F = 14.71 kN
19.Pipe friction & head loss

Answer: hf = 1.301 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·0.2²/4 = 0.03142 m²
V = Q/A = 0.06/0.03142 = 1.91 m/s

Velocity head

V²/(2g) = 1.91²/(2·9.81) = 0.1859 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.028·(50/0.2)·1.91²/(2·9.81) = 1.301 m

Answer

hf = 1.301 m
20.Pipe friction & head loss

Answer: H = 3.503 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 = 0.04/0.03142 = 1.273 m/s
V²/(2g) = 0.08263 m

Loss coefficients

f·L/D = 0.015·400/0.2 = 30
ΣK = 0.5 + 3·0.3 + 10 = 11.4

Energy equation

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

H = (1 + 30 + 11.4)·0.08263 = 3.503 m

Answer

H = 3.503 m
21.Open-channel flow (Manning)

Answer: Q = 1.99 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 + z·y)·y = (5 + 3·0.5)·0.5 = 3.25 m²
P = b + 2y·√(1 + z²) = 5 + 2·0.5·√(1 + 3²) = 8.162 m
R = A/P = 0.3982 m

Velocity

V = (1/0.025)·0.39822/3·0.00081/2 = 0.6123 m/s

Flow rate

Q = A·V = 3.25·0.6123 = 1.99 m³/s

Answer

Q = 1.99 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002848 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 = 2.5·1.9 = 4.75 m²
P = b + 2y = 2.5 + 2·1.9 = 6.3 m
R = A/P = 0.754 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.014·15/(4.75·0.8284) = 0.05337
S = 0.05337² = 0.002848

Answer

S = 0.002848

That is a fall of 2.848 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 25.9 kW

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

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.03·66 = 19.42 kW

Shaft power

Pshaft = Ph/η = 19.42/0.75 = 25.9 kW

Answer

Pshaft = 25.9 kW
24.Pumps & pump power

Answer: H = 20.9 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 = 0.08/0.03142 = 2.546 m/s
V²/(2g) = 0.3305 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (30 + 6)·0.3305 = 11.9 m

Pump head

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

H = Δz + hL = 9 + 11.9 = 20.9 m

Answer

H = 20.9 m
25.Time value of money

Answer: PV = 17914 €

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.

Annuity factor

(1 − (1 + i)−n)/i = (1 − 0.582)/0.07 = 5.971

Present value

PV = 3 000·5.971 = €17 913.90

Answer

PV = €17 913.90
26.Time value of money

Answer: A = 371.6 €

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 payments

i = 0.07200000000000001/12 = 0.006
N = 12·3 = 36

Payment

The present value of N equal payments A is A·(1 − (1 + i)⁻ᴺ)/i. Set it equal to the loan and solve for A.

(1 + i)−N = 0.8063
A = 12 000·0.006/(1 − 0.8063) = €371.62

Answer

A = €371.62
27.NPV & IRR

Answer: NPV = 11111 €

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.

Value of the cash flows

PV = 10 000/(0.1 − 0.01) = 111 111.11

NPV

NPV = 111 111.11 − 100 000 = €11 111.11

Answer

NPV = €11 111.11

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

28.NPV & IRR

Answer: IRR = 23.25 %

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(20%) = 1 284.72
NPV(25%) = −648.00

Narrow down

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

IRR ≈ 20 + 5·1 284.72/(1 284.72 − (−648.00)) = 23.32%
exact: NPV(23.25%) = 0 → IRR = 23.25%

Answer

IRR = 23.25%
29.Normal distribution

Answer: z = 0.77

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 + 0.5587)/2 = 0.7794

Read the z-table backwards

Find 0.7794 inside the table and read off z.

z = 0.77

Answer

z = 0.77
30.Normal distribution

Answer: x = 253.4 g

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) = 0.75

z from the table

z ≈ 0.67

Back to the original units

x = 250 + 0.67·5 = 253.4 g

Answer

x = 253.4 g

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