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​ = 15 kNP2​ = 15 kNABRA​RB​ = ?1 m6 m1 m

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

L = 8 mP1 = 15 kN at 1 mP2 = 15 kN at 7 m
RB = kN
2.Beam support reactionsHard
w = 5 kN/mP = 25 kNABRA​ = ?RB​3 m1 m2 m

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

L = 6 mP = 25 kN at 4 mw = 5 kN/m from 0 to 3 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB10 kN4 m3 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 3 m from Avertical load = 10 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB40 kN25 kN6 m4 m2 m

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

span = 6 mheight = 2 mB is 4 m from Avertical load = 40 kNhorizontal load = 25 kN →
FAC = kN
5.Shear force & bending momentMedium
w = 4 kN/mABsection5.5 m2.5 m

Find the bending moment Mx at the section x = 5.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mw = 4 kN/m from 0 to 8 mx = 5.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 3 kN/mP = 45 kNABsection0.5 m5.5 m2 m

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

L = 8 mP = 45 kN at 6 mw = 3 kN/m from 0 to 8 mx = 0.5 m
Mx = kN·m
7.Beam deflectionMedium
w = 2 kN/mδL = 2 m

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

w = 2 kN/mL = 2 mE = 11 GPa (timber)I = 12 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
P = 24 kNABδ3 m1 m

A simply supported beam carries a point load P at b = 1 m from support B. Find the maximum deflection δmax of the beam.

P = 24 kNb = 1 mL = 4 mE = 70 GPa (aluminium)I = 23 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 3 md = 40 mmcross-section

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

L = 3 mE = 200 GPa (steel)d = 40 mm
Pcr = kN
10.Column bucklingHard
PL = 5 md = 80 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 = 5 mE = 200 GPa (steel)d = 80 mm
σcr = MPa
11.Centroid & second moment of areaMedium
B = 120H = 225t = 10xdimensions in mm

A hollow rectangular (box) section has outer width B = 120 mm, outer height H = 225 mm and a uniform wall thickness t = 10 mm. Find its radius of gyration r about the horizontal centroidal axis.

B = 120 mmH = 225 mmt = 10 mm
r = mm
12.Centroid & second moment of areaHard
2403030010xM = 5 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 5 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 240 mmtf = 30 mmtw = 10 mmhw = 300 mmM = 5 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 19 kN/m³10 mwater tableXz = 4 m

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

z = 4 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 19 kN/m³
σ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 20 kN/m³3 mclayγsat​ = 19 kN/m³8 mwater tableXz = 7 m

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

z = 7 mzw = 2 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 20 kN/m³clay: γsat = 19 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 25 kPasandclayCc​ = 0.3, Cr​ = 0.06e0​ = 0.7σ′0​ = 45 kPaσ′p​ = 85 kPa7 mwater table

A 7 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 85 kPa. A new building adds 25 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7 mCc = 0.3Cr = 0.06e0 = 0.7σ′0 = 45 kPaσ′p = 85 kPaΔσ = 25 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 10 mcv​ = 4 m²/year10 msandwater table

A clay layer 10 m thick has a coefficient of consolidation cv = 4 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 70% average consolidation the time factor is Tv = 0.403. How many years t does the layer take to reach 70% consolidation?

H = 10 mcv = 4 m²/yearU = 70%Tv = 0.403double drainage
t = years
17.Hydrostatic forceMedium
gated = 4 mH = 2 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 2 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 4 mH = 2 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 4 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 4 mH = 2 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 1.7 m/sD = 200 mmL = 400 mf = 0.03

Water flows at a mean velocity of 1.7 m/s through a pipe 400 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

V = 1.7 m/sL = 400 mD = 200 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10free outletH = ?L = 200 m, D = 300 mm, f = 0.0154× bend (K = 0.3)

A pipe 200 m long with an inside diameter of 300 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), 4 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 100 L/s?

Q = 100 L/sL = 200 mD = 300 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10
H = m
21.Open-channel flow (Manning)Medium
b = 6 my = 1.8 mn = 0.015, S = 0.005

A rectangular brickwork channel is 6 m wide. Water flows uniformly 1.8 m deep. Manning n = 0.015 and the bed slope is S = 0.005. Find the flow rate Q in m³/s.

b = 6 my = 1.8 mn = 0.015S = 0.005
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 250 mmn = 0.013, V = 0.6 m/s

A concrete sewer with an inside diameter of 250 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.6 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 250 mmn = 0.013V = 0.6 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 40 L/sH = 68 m

In a test, a pump delivers 40 L/s of water (ρ = 1000 kg/m³) against a head of 68 m while its shaft takes 31.4 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 40 L/sH = 68 mPshaft = 31.4 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
150 kPa (gauge)PQ = 50 L/sΔz = 12 mL = 200 m, D = 200 mm, f = 0.02, ΣK = 8

A pump moves 50 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 12 m higher. The pipe is 200 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 = 8 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 150 kPa. Find the head H the pump must add.

Q = 50 L/sΔz = 12 mL = 200 mD = 200 mmf = 0.02ΣK = 8ptank = 150 kPa
H = m
25.Time value of moneyMedium
periods0123411 + EAR = ?25% / 4

A credit card charges a nominal interest rate of 25% per year, compounded quarterly. Find the effective annual rate EAR in percent.

r = 25%m = 4
EAR = %
26.Time value of moneyHard
months0123…228€150€150€150FV = ?

You save €150 at the end of every month for 19 years. The account pays 6% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €1506% / 12N = 228
FV = €
27.NPV & IRRMedium
years01234−75 00019 00022 00017 00033 000

An investment of €75 000 gives these cash flows at the end of years 1 to 4: €19 000, €22 000, €17 000, €33 000. The cost of capital is 6%. Find the net present value NPV.

r = 6%CF0 = −75 000CF1 = 19 000CF2 = 22 000CF3 = 17 000CF4 = 33 000
NPV = €
28.NPV & IRRHard
years0123−40 00024 50028 50015 000

A project costs €40 000 and returns €24 500, €28 500, €15 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 24 500CF2 = 28 500CF3 = 15 000
IRR = %
29.Normal distributionMedium
488548P = ?

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. What fraction lies between 488 and 548 h? Give P as a decimal.

μ = 500σ = 40x1 = 488x2 = 548
P =
30.Normal distributionHard
0.04 mm0D − d?

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

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

3Solutions

1.Beam support reactions

Answer: RB = 15 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​ = 15 kNP2​ = 15 kNABRA​RB​1 m6 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 = 15·1 + 15·7
RB = 120/8 = 15 kN
ΣFy = 0: RA = 30 − 15 = 15 kN

Answer

RB = 15 kN
2.Beam support reactions

Answer: RA = 19.58 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 = 5 kN/mP = 25 kNABRA​RB​3 m1 m2 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 = 5·3 = 15 kN, acting at x̄ = 1.5 m
ΣMA = 0: RB·6 = 25·4 + 5·3·1.5
RB = 122.5/6 = 20.42 kN
ΣFy = 0: RA = 40 − 20.42 = 19.58 kN

Answer

RA = 19.58 kN
3.Truss: method of joints

Answer: FAB = −4.507 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.

ABBCACACB10 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·4 = 10·3 → Cy = 7.5 kN
ΣFy = 0: Ay = 10 − 7.5 = 2.5 kN

Joint A

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

sin α = 2/3.606 = 0.5547
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −2.5/0.5547 = −4.507 kN

Answer

FAB = −4.507 kN (compression)
4.Truss: method of joints

Answer: FAC = 35 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 kN25 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 40·4 + 25·2 → Cy = 35 kN
ΣFy = 0: Ay = 40 − 35 = 5 kN
ΣFx = 0: Ax = −25 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 = 2/2.828 = 0.7071, cos γ = 2/2.828 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −35/0.7071 = −49.5 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−49.5)·0.7071 = 35 kN

Answer

FAC = 35 kN (tension)
5.Shear force & bending moment

Answer: Mx = 27.5 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 = 4·8 = 32 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 4·8·4
RB = 128/8 = 16 kN
ΣFy = 0: RA = 32 − 16 = 16 kN
w = 4 kN/mABRA​ = 16RB​ = 16section5.5 m2.5 m

Cut at x = 5.5 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 = 16·5.5 − 4·5.5·2.75 = 27.5 kN·m

Answer

Mx = 27.5 kN·m
6.Shear force & bending moment

Answer: Mx = 11.25 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 = 3·8 = 24 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 45·6 + 3·8·4
RB = 366/8 = 45.75 kN
ΣFy = 0: RA = 69 − 45.75 = 23.25 kN
w = 3 kN/mP = 45 kNABRA​ = 23.25RB​ = 45.75section0.5 m5.5 m2 m

Cut at x = 0.5 m and keep the left part

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

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 23.25·0.5 − 3·0.5·0.25 = 11.25 kN·m

Answer

Mx = 11.25 kN·m
7.Beam deflection

Answer: δmax = 3.157 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 = 2 N/mm, L = 2000 mm
EI = 1.32 × 10¹¹ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·2·2000⁴/(384·1.32 × 10¹¹) = 3.157 mm

Answer

δmax = 3.157 mm
8.Beam deflection

Answer: δmax = 13.89 mm

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

Consistent units

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

P = 24000 N, b = 1000 mm, L = 4000 mm
EI = 1.61 × 10¹² N·mm²

Position of the maximum

Setting the slope in the longer segment to zero gives the position.

x = √((L² − b²)/3) = √((4000² − 1000²)/3) = 2236 mm

Maximum deflection

δmax = Pb(L² − b²)3/2/(9√3·EIL) = 13.89 mm

Answer

δmax = 13.89 mm
9.Column buckling

Answer: Pcr = 110.2 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·40⁴/64 = 125664 mm⁴

Effective length

KL = 0.5·3000 = 1500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·125664/1500² = 110245 N = 110.2 kN

Answer

Pcr = 110.2 kN
10.Column buckling

Answer: σcr = 126.3 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·80⁴/64 = 2.011 × 10⁶ mm⁴

Radius of gyration and slenderness

A = 5027 mm²
r = √(I/A) = √(2.011 × 10⁶/5027) = 20 mm
KL = 0.5·5000 = 2500 mm
KL/r = 2500/20 = 125

Critical stress

σcr = π²E/(KL/r)² = π²·200000/125² = 126.3 MPa

Answer

σcr = 126.3 MPa
11.Centroid & second moment of area

Answer: r = 80.49 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

b = 100 mm, h = 205 mm
A = BH − bh = 120·225 − 100·205 = 6500 mm²
I = (BH³ − bh³)/12 = 4.211 × 10⁷ mm⁴

Radius of gyration

r = √(I/A) = √(4.211 × 10⁷/6500) = 80.49 mm

Answer

r = 80.49 mm
12.Centroid & second moment of area

Answer: σbottom = 16.51 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 = 240·30 = 7200 mm², yf = 300 + 30/2 = 315 mm
web: Aw = 10·300 = 3000 mm², yw = 300/2 = 150 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (7200·315 + 3000·150)/10200 = 266.5 mm

Parallel-axis theorem

flange: 240·30³/12 + 7200·(315 − 266.5)² = 1.75 × 10⁷ mm⁴
web: 10·300³/12 + 3000·(150 − 266.5)² = 6.32 × 10⁷ mm⁴
Ix = 1.75 × 10⁷ + 6.32 × 10⁷ = 8.069 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 266.5 mm
σ = M·y/I = 5 × 10⁶·266.5/8.069 × 10⁷ = 16.51 MPa

Answer

σbottom = 16.51 MPa
13.Effective stress in soil

Answer: σ = 65.5 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) = 15.5·3 + 19·1 = 65.5 kPa

Answer

σ = 65.5 kPa
14.Effective stress in soil

Answer: σ′ = 77.95 kPa

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

Total stress

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

σ = γd·2 + γsat,sand·1 + γsat,clay·4
σ = 15.5·2 + 20·1 + 19·4 = 127 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 = 127 − 49.05 = 77.95 kPa

Answer

σ′ = 77.95 kPa
15.Consolidation settlement

Answer: S = 47.41 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 + 25 = 70 kPa ≤ 85 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.06·7/(1 + 0.7)·log₁₀(70/45) = 47.41 mm

Answer

S = 47.41 mm
16.Consolidation settlement

Answer: t = 2.519 years

Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.

Drainage path

Hdr = H/2 = 10/2 = 5 m

Time

t = Tv·Hdr²/cv = 0.403·5²/4 = 2.519 years

Answer

t = 2.519 years
17.Hydrostatic force

Answer: F = 294.3 kN

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

Centroid depth and area

yc = d + H/2 = 4 + 2/2 = 5 m
A = H·b = 2·3 = 6 m²
gated = 4 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·5·6 = 294.3 kN

Answer

F = 294.3 kN
18.Hydrostatic force

Answer: ycp = 5.067 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 = 4 + 2/2 = 5 m
A = H·b = 2·3 = 6 m²
gated = 4 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·5·6 = 294.3 kN

Centre of pressure

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

Ic = b·H³/12 = 3·2³/12 = 2 m⁴
ycp = yc + Ic/(yc·A) = 5 + 2/(5·6) = 5.067 m

Answer

ycp = 5.067 m
19.Pipe friction & head loss

Answer: hf = 8.838 m

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

Velocity head

V²/(2g) = 1.7²/(2·9.81) = 0.1473 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(400/0.2)·1.7²/(2·9.81) = 8.838 m

Answer

hf = 8.838 m
20.Pipe friction & head loss

Answer: H = 2.316 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 = 0.015·200/0.3 = 10
ΣK = 0.5 + 4·0.3 + 10 = 11.7

Energy equation

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

H = (1 + 10 + 11.7)·0.102 = 2.316 m

Answer

H = 2.316 m
21.Open-channel flow (Manning)

Answer: Q = 55.07 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 = 6·1.8 = 10.8 m²
P = b + 2y = 6 + 2·1.8 = 9.6 m
R = A/P = 1.125 m

Velocity

V = (1/0.015)·1.1252/3·0.0051/2 = 5.099 m/s

Flow rate

Q = A·V = 10.8·5.099 = 55.07 m³/s

Answer

Q = 55.07 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002453 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.

Hydraulic radius

R = D/4 = 0.25/4 = 0.0625 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.6/0.1575)² = 0.002453

Answer

S = 0.002453

That is a fall of 2.453 m per kilometre.

23.Pumps & pump power

Answer: η = 84.98 %

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 = 1000·9.81·0.04·68 = 26.68 kW

Efficiency

η = Ph/Pshaft = 26.68/31.4 = 84.98%

Answer

η = 84.98%
24.Pumps & pump power

Answer: H = 30.91 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 = 0.05/0.03142 = 1.592 m/s
V²/(2g) = 0.1291 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (20 + 8)·0.1291 = 3.615 m

Pressure head

p/(ρ·g) = 150000/(1000·9.81) = 15.29 m

Pump head

Both surfaces are practically at rest, so there is no velocity head term.

H = Δz + p/(ρ·g) + hL = 12 + 15.29 + 3.615 = 30.91 m

Answer

H = 30.91 m
25.Time value of money

Answer: EAR = 27.44 %

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

Rate per period

r/m = 0.25/4 = 0.0625

Compound over one year

EAR = (1 + 0.0625)4 − 1 = 1.274 − 1 = 27.44%

Answer

EAR = 27.44%

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

26.Time value of money

Answer: FV = 63537 €

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 = 0.06/12 = 0.005
N = 12·19 = 228

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 150·(3.118 − 1)/0.005 = €63 536.98

Answer

FV = €63 536.98

You paid in €34 200 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = 2917 €

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 = −75 000
CF1/(1 + 0.06)1 = 19 000/1.06 = 17 924.53
CF2/(1 + 0.06)2 = 22 000/1.124 = 19 579.92
CF3/(1 + 0.06)3 = 17 000/1.191 = 14 273.53
CF4/(1 + 0.06)4 = 33 000/1.262 = 26 139.09

Add them up

NPV = €2 917.07

Answer

NPV = €2 917.07

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

28.NPV & IRR

Answer: IRR = 34.77 %

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(30%) = 2 537.55
NPV(35%) = −117.36

Narrow down

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

IRR ≈ 30 + 5·2 537.55/(2 537.55 − (−117.36)) = 34.78%
exact: NPV(34.77%) = 0 → IRR = 34.77%

Answer

IRR = 34.77%
29.Normal distribution

Answer: P = 0.5028

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-scores

z₁ = (488 − 500)/40 = −0.3
z₂ = (548 − 500)/40 = 1.2

Area between

P = Φ(1.2) − Φ(−0.3) = 0.8849 − 0.3821 = 0.5028

Answer

P = 0.5028
30.Normal distribution

Answer: P = 0.9207

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

Distribution of the difference

μ = 25.04 − 25 = 0.04 mm, σ = 0.02828 mm

Standardise

z = (0 − 0.04)/0.02828 = −1.41

Probability

P = 1 − Φ(−1.41) = 0.9207

Answer

P = 0.9207

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