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​ = 40 kNP2​ = 15 kNABRA​ = ?RB​1 m3.5 m1.5 m

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

L = 6 mP1 = 40 kN at 1 mP2 = 15 kN at 4.5 m
RA = kN
2.Beam support reactionsHard
w = 3 kN/mP = 35 kNABRA​RB​ = ?1 m5 m3 m1 m

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

L = 10 mP = 35 kN at 1 mw = 3 kN/m from 6 to 9 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB40 kN8 m3 m3 m

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

span = 8 mheight = 3 mB is 3 m from Avertical load = 40 kN
FAC = kN
4.Truss: method of jointsHard
ABBCACACB55 kN20 kN8 m5 m2 m

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

span = 8 mheight = 2 mB is 5 m from Avertical load = 55 kNhorizontal load = 20 kN →
FAB = kN
5.Shear force & bending momentMedium
w = 10 kN/mABsection0.5 m3.5 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 = 4 mw = 10 kN/m from 0 to 4 mx = 0.5 m
Mx = kN·m
6.Shear force & bending momentHard
4 kN/m35 kN55 kN60 kNABCDEFG1 m1 m1 m1 m1 m1 m

The marks A to G split the beam into six equal parts. At which mark is the bending moment largest in size, sagging or hogging? Click it in the diagram.

35 kN @ 0 m55 kN @ 6 m60 kN @ 2 m4 kN/m, 1–4 m
  1. 1A (x = 0 m)
  2. 2B (x = 1 m)
  3. 3C (x = 2 m)
  4. 4D (x = 3 m)
  5. 5E (x = 4 m)
  6. 6F (x = 5 m)
  7. 7G (x = 6 m)
7.Beam deflectionMedium
w = 4 kN/mδL = 4 m

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

w = 4 kN/mL = 4 mE = 200 GPa (steel)I = 23 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
P = 26 kNABδ3.5 m1.5 m

A simply supported beam carries a point load P at b = 1.5 m from support B. Find the maximum deflection δmax of the beam.

P = 26 kNb = 1.5 mL = 5 mE = 11 GPa (timber)I = 160 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 5 md = 30 mmcross-section

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

L = 5 mE = 70 GPa (aluminium)d = 30 mm
Pcr = kN
10.Column bucklingHard
P = 145 kNL = 6 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and pinned at the top. It must carry 145 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 145 kNn = 2.5L = 6 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
120 mm150 mm105 mmØ50xIx​ = ?

A 120 mm × 150 mm plate has a circular hole of diameter 50 mm on its vertical centre line, with its centre 105 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 120 mmh = 150 mmd = 50 mmhole centre: y = 105 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1001010014xM = 15 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 15 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 100 mmtf = 10 mmtw = 14 mmhw = 100 mmM = 15 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 17 kN/m³γsat​ = 19.5 kN/m³14 mwater tableXz = 14 m

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

z = 14 mzw = 2 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16.5 kN/m³γsat​ = 20 kN/m³3 mclayγsat​ = 18.5 kN/m³7 mwater tableXz = 6.5 m

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

z = 6.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 20 kN/m³clay: γsat = 18.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 130 kPasandclayCc​ = 0.3, Cr​ = 0.03e0​ = 0.95σ′0​ = 45 kPaσ′p​ = 85 kPa8 mwater table

An 8 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.03 and e₀ = 0.95. At its mid-depth the effective vertical stress is 45 kPa and the preconsolidation pressure is 85 kPa. A new building adds 130 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 8 mCc = 0.3Cr = 0.03e0 = 0.95σ′0 = 45 kPaσ′p = 85 kPaΔσ = 130 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 10 mcv​ = 1.2 m²/year10 mimpervious rockwater table

A clay layer 10 m thick has a coefficient of consolidation cv = 1.2 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 90% average consolidation the time factor is Tv = 0.848. How many years t does the layer take to reach 90% consolidation?

H = 10 mcv = 1.2 m²/yearU = 90%Tv = 0.848single drainage
t = years
17.Hydrostatic forceMedium
gated = 2.5 mH = 2 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 resultant hydrostatic force F on the gate.

d = 2.5 mH = 2 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 0.5 mH = 1.5 m

A vertical rectangular gate 2 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 = 1.5 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 3 m/sD = 100 mmL = 300 mf = 0.03

Water flows at a mean velocity of 3 m/s through a pipe 300 m long with an inside diameter of 100 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

V = 3 m/sL = 300 mD = 100 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2Δz = ?L = 200 m, D = 150 mm, f = 0.0183× bend (K = 0.3)

Two open reservoirs are joined by a pipe 200 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.018. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each), a valve (K = 2) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². What difference in water level Δz between the reservoirs gives a flow rate of 30 L/s?

Q = 30 L/sL = 200 mD = 150 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 2Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 6 my = 2.1 m3 : 1n = 0.012, S = 0.0005

A trapezoidal finished concrete channel has a bottom width of 6 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 2.1 m deep. Manning n = 0.012 and the bed slope is S = 0.0005. Find the flow rate Q in m³/s.

b = 6 my = 2.1 mz = 3n = 0.012S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 600 mmn = 0.013, V = 1 m/s

A concrete sewer with an inside diameter of 600 mm (Manning n = 0.013) must reach a self-cleansing velocity of 1 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 600 mmn = 0.013V = 1 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 150 L/sH = 52 m

In a test, a pump delivers 150 L/s of water (ρ = 1000 kg/m³) against a head of 52 m while its shaft takes 95.6 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 150 L/sH = 52 mPshaft = 95.6 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 50 L/sΔz = 8 mL = 400 m, D = 200 mm, f = 0.018, ΣK = 6

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 8 m higher. The pipe is 400 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.018; 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 = 50 L/sΔz = 8 mL = 400 mD = 200 mmf = 0.018ΣK = 6
H = m
25.Time value of moneyMedium
years01234€3 000FV = ?

You invest €3 000 at a nominal rate of 3.6% per year, compounded quarterly. Find the value FV of the investment after 4 years.

PV = €3 0003.6% / 4n = 4
FV = €
26.Time value of moneyHard
months01…276…360€300 000AB = ?A7.2% / 12

A mortgage of €300 000 is repaid with equal monthly payments over 30 years at 7.2% per year, compounded monthly. How much is still owed just after the payment at the end of year 23? Find the outstanding balance B.

P = €300 0007.2% / 12N = 360k = 276
B = €
27.NPV & IRRMedium
years0123−75 00033 00020 00030 000

An investment of €75 000 gives these cash flows at the end of years 1 to 3: €33 000, €20 000, €30 000. The cost of capital is 7.000000000000001%. Find the net present value NPV.

r = 7.000000000000001%CF0 = −75 000CF1 = 33 000CF2 = 20 000CF3 = 30 000
NPV = €
28.NPV & IRRHard
years012−10 0004 0007 500

A project costs €10 000 and returns €4 000, €7 500 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −10 000CF1 = 4 000CF2 = 7 500
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area to the right of z = 0.1685

Drag z so that the shaded area under the standard normal curve, to the right of z, is 0.1685. Find z to two decimals.

A = 0.1685
z =
30.Normal distributionHard
4 s0X − Y?

Runner A's lap time X and runner B's lap time Y are independent and normal: X has mean 52 s and standard deviation 4 s, Y has mean 48 s and standard deviation 3 s. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 52 s, σX = 4 sμY = 48 s, σY = 3 s
P =

3Solutions

1.Beam support reactions

Answer: RA = 37.08 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​ = 40 kNP2​ = 15 kNABRA​RB​1 m3.5 m1.5 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·6 = 40·1 + 15·4.5
RB = 107.5/6 = 17.92 kN
ΣFy = 0: RA = 55 − 17.92 = 37.08 kN

Answer

RA = 37.08 kN
2.Beam support reactions

Answer: RB = 10.25 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 = 3 kN/mP = 35 kNABRA​RB​1 m5 m3 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 = 3·3 = 9 kN, acting at x̄ = 7.5 m
ΣMA = 0: RB·10 = 35·1 + 3·3·7.5
RB = 102.5/10 = 10.25 kN
ΣFy = 0: RA = 44 − 10.25 = 33.75 kN

Answer

RB = 10.25 kN
3.Truss: method of joints

Answer: FAC = 25 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·8 = 40·3 → Cy = 15 kN
ΣFy = 0: Ay = 40 − 15 = 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 = 3/5.831 = 0.5145, cos γ = 5/5.831 = 0.8575
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −15/0.5145 = −29.15 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−29.15)·0.8575 = 25 kN

Answer

FAC = 25 kN (tension)
4.Truss: method of joints

Answer: FAB = −42.07 kN

Method of joints: every pin of a truss is in equilibrium, so ΣFx = 0 and ΣFy = 0 at each joint. Start at a joint with at most two unknown member forces. A negative result means the member is in compression.

ABBCACACB55 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 55·5 + 20·2 → Cy = 39.38 kN
ΣFy = 0: Ay = 55 − 39.38 = 15.63 kN
ΣFx = 0: Ax = −20 kN

Joint A

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

sin α = 2/5.385 = 0.3714
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −15.63/0.3714 = −42.07 kN

Answer

FAB = −42.07 kN (compression)
5.Shear force & bending moment

Answer: Mx = 8.75 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 = 10·4 = 40 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 10·4·2
RB = 80/4 = 20 kN
ΣFy = 0: RA = 40 − 20 = 20 kN
w = 10 kN/mABRA​ = 20RB​ = 20section0.5 m3.5 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 = 20·0.5 − 10·0.5·0.25 = 8.75 kN·m

Answer

Mx = 8.75 kN·m
6.Shear force & bending moment

Answer: E (x = 4 m)

Largest bending moment: M changes slope wherever the shear force changes, so its peaks sit where the shear force crosses zero: under a point load, inside a distributed load, or over a support of an overhang. At a fixed support of a cantilever the moment is largest at the wall. Compare the size of M at those places, sagging or hogging.

Support reactions

Take moments about one support, then use the vertical force balance.

R1 = 56 kN, R2 = 106 kN

Bending moment at every mark

Sum the moments of all forces on one side of the cut. Sagging is positive, hogging negative.

MA = 0, MB = −35, MC = −16, MD = −61, ME = −110 kN·m, MF = −55, MG = 0

Answer

Mark E: ME = −110 kN·m
7.Beam deflection

Answer: δmax = 2.899 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 = 4000 mm
EI = 4.6 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·4·4000⁴/(384·4.6 × 10¹²) = 2.899 mm

Answer

δmax = 2.899 mm
8.Beam deflection

Answer: δmax = 30.85 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 = 26000 N, b = 1500 mm, L = 5000 mm
EI = 1.76 × 10¹² N·mm²

Position of the maximum

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

x = √((L² − b²)/3) = √((5000² − 1500²)/3) = 2754 mm

Maximum deflection

δmax = Pb(L² − b²)3/2/(9√3·EIL) = 30.85 mm

Answer

δmax = 30.85 mm
9.Column buckling

Answer: Pcr = 4.395 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·30⁴/64 = 39761 mm⁴

Effective length

KL = 0.5·5000 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·39761/2500² = 4395 N = 4.395 kN

Answer

Pcr = 4.395 kN
10.Column buckling

Answer: d = 90.13 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 = 2.5·145000 = 362500 N
KL = 0.7·6000 = 4200 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·362500·4200²/(π³·200000))^(1/4) = 90.13 mm

Answer

d = 90.13 mm

Check: the slenderness KL/r is 186.4, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 31.46 × 10⁶ mm⁴

Sections with holes: treat a hole as a negative area. The centroid is ȳ = (A₁y₁ − A₂y₂)/(A₁ − A₂), with A₁, y₁ for the full plate and A₂, y₂ for the hole. For the second moment of area about the centroidal axis, use the parallel-axis theorem for each part and subtract the hole: I = (Ic1 + A₁d₁²) − (Ic2 + A₂d₂²), where d is the distance from each part's own centroid to the axis through ȳ. A rectangle has Ic = bh³/12 and a circle Ic = πd⁴/64.

Centroid

ȳ = (18000·75 − 1963·105)/(18000 − 1963) = 71.33 mm

Full plate about ȳ

120·150³/12 + 18000·3.673² = 33.99 × 10⁶ mm⁴

Hole about ȳ

π·50⁴/64 + 1963·33.67² = 2.533 × 10⁶ mm⁴

Subtract

Ix = 31.46 × 10⁶ mm⁴

Answer

Ix = 31.46 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 189.2 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 = 100·10 = 1000 mm², yf = 100 + 10/2 = 105 mm
web: Aw = 14·100 = 1400 mm², yw = 100/2 = 50 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (1000·105 + 1400·50)/2400 = 72.92 mm

Parallel-axis theorem

flange: 100·10³/12 + 1000·(105 − 72.92)² = 1.038 × 10⁶ mm⁴
web: 14·100³/12 + 1400·(50 − 72.92)² = 1.902 × 10⁶ mm⁴
Ix = 1.038 × 10⁶ + 1.902 × 10⁶ = 2.94 × 10⁶ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 110 − 72.92 = 37.08 mm
σ = M·y/I = 1.5 × 10⁷·37.08/2.94 × 10⁶ = 189.2 MPa

Answer

σtop = 189.2 MPa
13.Effective stress in soil

Answer: σ′ = 150.3 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) = 17·2 + 19.5·12 = 268 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·12 = 117.7 kPa

Effective stress

σ′ = σ − u = 268 − 117.7 = 150.3 kPa

Answer

σ′ = 150.3 kPa
14.Effective stress in soil

Answer: σ′ = 73.6 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·3.5
σ = 16.5·2 + 20·1 + 18.5·3.5 = 117.8 kPa

Pore water pressure

Water pressure grows with depth below the water table.

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

Effective stress

σ′ = σ − u = 117.8 − 44.15 = 73.6 kPa

Answer

σ′ = 73.6 kPa
15.Consolidation settlement

Answer: S = 420 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 + 130 = 175 kPa > 85 kPa

Settlement

Recompression up to σ′p, virgin compression beyond it.

S = 0.03·8/(1 + 0.95)·log₁₀(85/45) + 0.3·8/(1 + 0.95)·log₁₀(175/85)
S = 33.99 + 386 = 420 mm

Answer

S = 420 mm
16.Consolidation settlement

Answer: t = 70.67 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 = 10 m

Time

t = Tv·Hdr²/cv = 0.848·10²/1.2 = 70.67 years

Answer

t = 70.67 years
17.Hydrostatic force

Answer: F = 103 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 = 2.5 + 2/2 = 3.5 m
A = H·b = 2·1.5 = 3 m²
gated = 2.5 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.5·3 = 103 kN

Answer

F = 103 kN
18.Hydrostatic force

Answer: F = 36.79 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 + 1.5/2 = 1.25 m
A = H·b = 1.5·2 = 3 m²
gated = 0.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·1.25·3 = 36.79 kN

Answer

F = 36.79 kN
19.Pipe friction & head loss

Answer: hf = 41.28 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) = 3²/(2·9.81) = 0.4587 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(300/0.1)·3²/(2·9.81) = 41.28 m

Answer

hf = 41.28 m
20.Pipe friction & head loss

Answer: Δz = 4.172 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 = 0.03/0.01767 = 1.698 m/s
V²/(2g) = 0.1469 m

Loss coefficients

f·L/D = 0.018·200/0.15 = 24
ΣK = 0.5 + 3·0.3 + 2 + 1.0 = 4.4

Total head loss

hf = 24·0.1469 = 3.525 m
hm = 4.4·0.1469 = 0.6463 m
Δz = hf + hm = 4.172 m

Answer

Δz = 4.172 m
21.Open-channel flow (Manning)

Answer: Q = 58.49 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 = (6 + 3·2.1)·2.1 = 25.83 m²
P = b + 2y·√(1 + z²) = 6 + 2·2.1·√(1 + 3²) = 19.28 m
R = A/P = 1.34 m

Velocity

V = (1/0.012)·1.342/3·0.00051/2 = 2.264 m/s

Flow rate

Q = A·V = 25.83·2.264 = 58.49 m³/s

Answer

Q = 58.49 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.00212 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 = 0.6/4 = 0.15 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·1/0.2823)² = 0.00212

Answer

S = 0.00212

That is a fall of 2.12 m per kilometre.

23.Pumps & pump power

Answer: η = 80.04 %

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 = 1000·9.81·0.15·52 = 76.52 kW

Efficiency

η = Ph/Pshaft = 76.52/95.6 = 80.04%

Answer

η = 80.04%
24.Pumps & pump power

Answer: H = 13.42 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) = (36 + 6)·0.1291 = 5.422 m

Pump head

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

H = Δz + hL = 8 + 5.422 = 13.42 m

Answer

H = 13.42 m
25.Time value of money

Answer: FV = 3462 €

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

Rate and number of periods

i = r/m = 0.036000000000000004/4 = 0.009
N = m·n = 4·4 = 16

Future value

FV = 3 000·(1 + 0.009)16 = 3 000·1.154 = €3 462.42

Answer

FV = €3 462.42
26.Time value of money

Answer: B = 134054 €

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 payment

i = 0.006, N = 360
A = 300 000·0.006/(1 − (1 + 0.006)−360) = €2 036.36

Present value of the remaining payments

Whatever is still owed must be exactly paid off by the remaining payments.

N − k = 360 − 276 = 84
B = 2036·(1 − (1 + 0.006)−84)/0.006 = €134 053.94

Answer

B = €134 053.94
27.NPV & IRR

Answer: NPV = −2201 €

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 + 0.07)1 = 33 000/1.07 = 30 841.12
CF2/(1 + 0.07)2 = 20 000/1.145 = 17 468.77
CF3/(1 + 0.07)3 = 30 000/1.225 = 24 488.94

Add them up

NPV = €−2 201.17

Answer

NPV = €−2 201.17

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

28.NPV & IRR

Answer: IRR = 8.882 %

Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.

Bracket the IRR

NPV falls as the rate rises, so the IRR lies between a rate with positive NPV and one with negative NPV.

NPV(5%) = 612.24
NPV(10%) = −165.29

Narrow down

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

IRR ≈ 5 + 5·612.24/(612.24 − (−165.29)) = 8.937%
exact: NPV(8.882%) = 0 → IRR = 8.882%

Answer

IRR = 8.882%
29.Normal distribution

Answer: z = 0.96

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 − 0.1685 = 0.8315

Read the z-table backwards

Find 0.8315 inside the table and read off z.

z = 0.96

Answer

z = 0.96
30.Normal distribution

Answer: P = 0.7881

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 = 52 − 48 = 4 s, σ = 5 s

Standardise

z = (0 − 4)/5 = −0.8

Probability

P = 1 − Φ(−0.8) = 0.7881

Answer

P = 0.7881

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