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​ = 25 kNP2​ = 25 kNABRA​ = ?RB​2 m0.5 m1.5 m

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

L = 4 mP1 = 25 kN at 2 mP2 = 25 kN at 2.5 m
RA = kN
2.Beam support reactionsHard
w = 10 kN/mP = 40 kNABRA​ = ?RB​2 m3 m3 m

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

L = 8 mP = 40 kN at 2 mw = 10 kN/m from 2 to 5 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB60 kN5 m3 m3 m

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

span = 5 mheight = 3 mB is 3 m from Avertical load = 60 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB15 kN5 kN8 m6 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 6 m from Avertical load = 15 kNhorizontal load = 5 kN →
FAC = kN
5.Shear force & bending momentMedium
5 kN/m20 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.

20 kN @ 3 m5 kN/m, 0–6 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)
6.Shear force & bending momentHard
8 kN/m35 kN55 kNABCDEFG2 m2 m2 m2 m2 m2 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 @ 12 m55 kN @ 4 m8 kN/m, 0–8 m
  1. 1A (x = 0 m)
  2. 2B (x = 2 m)
  3. 3C (x = 4 m)
  4. 4D (x = 6 m)
  5. 5E (x = 8 m)
  6. 6F (x = 10 m)
  7. 7G (x = 12 m)
7.Beam deflectionMedium
P = 24 kNABδ1 m1 m

A cantilever of length L is fixed at A and carries a point load P at a distance a = 1 m from A. Find the deflection δB at the free end B.

P = 24 kNa = 1 mL = 2 mE = 70 GPa (aluminium)I = 57 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
w = 4 kN/mAB6 m

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

L = 6 mw = 4 kN/m
RB = kN
9.Column bucklingMedium
PL = 3 m20 × 60 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)b × h = 20 × 60 mm
Pcr = kN
10.Column bucklingHard
P = 85 kNL = 2 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 85 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 85 kNn = 3L = 2 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
200120t = 10ȳ = ?dimensions in mm

A channel section lies with its open side up: a base plate 200 mm wide with two upright legs, 120 mm high overall. Base and legs are all 10 mm thick. Find the height ȳ of the centroid above the bottom edge.

b = 200 mmh = 120 mmt = 10 mm
ȳ = mm
12.Centroid & second moment of areaHard
2402014018xM = 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 = 240 mmtf = 20 mmtw = 18 mmhw = 140 mmM = 15 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 20 kN/m³14 mwater tableXz = 12 m

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

z = 12 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 20 kN/m³4 mclayγsat​ = 18 kN/m³5 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 = 15.5 kN/m³sand: γsat = 20 kN/m³clay: γsat = 18 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 200 kPasandclayCc​ = 0.2, Cr​ = 0.02e0​ = 0.95σ′0​ = 95 kPaσ′p​ = 195 kPa4 mwater table

A 4 m thick overconsolidated clay layer has Cc = 0.2, Cr = 0.02 and e₀ = 0.95. At its mid-depth the effective vertical stress is 95 kPa and the preconsolidation pressure is 195 kPa. A new building adds 200 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 4 mCc = 0.2Cr = 0.02e0 = 0.95σ′0 = 95 kPaσ′p = 195 kPaΔσ = 200 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 10 mcv​ = 0.8 m²/year10 mimpervious rockwater table

A clay layer 10 m thick has a coefficient of consolidation cv = 0.8 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 50% average consolidation the time factor is Tv = 0.197. How many years t does the layer take to reach 50% consolidation?

H = 10 mcv = 0.8 m²/yearU = 50%Tv = 0.197single drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 2.5 m

A vertical rectangular gate 1.5 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 = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 4 mH = 2.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of oil, with its top edge 4 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 4 mH = 2.5 mb = 2 mρ = 880 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 1.1 m/sD = 75 mmL = 100 mf = 0.025

Water (ρ = 1000 kg/m³) flows at 1.1 m/s through a horizontal pipe, 100 m long, with an inside diameter of 75 mm. Use the Darcy friction factor f = 0.025 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1.1 m/sL = 100 mD = 75 mmf = 0.025ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 2free outletH = ?L = 200 m, D = 300 mm, f = 0.0152× 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), 2 bends (K = 0.3 each) and a valve (K = 2). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 80 L/s?

Q = 80 L/sL = 200 mD = 300 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 2
H = m
21.Open-channel flow (Manning)Medium
b = 5 my = 0.6 m1 : 1n = 0.015, S = 0.0005

A trapezoidal brickwork channel has a bottom width of 5 m and side slopes of 1:1 (horizontal:vertical). Water flows uniformly 0.6 m deep. Manning n = 0.015 and the bed slope is S = 0.0005. Find the flow rate Q in m³/s.

b = 5 my = 0.6 mz = 1n = 0.015S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 6 my = 1.7 m1.5 : 1n = 0.012, Q = 43 m³/s

A trapezoidal finished concrete channel with a bottom width of 6 m and side slopes of 1.5:1 (horizontal:vertical) must carry 43 m³/s in uniform flow at a depth of 1.7 m. Manning n = 0.012. Find the required bed slope S (in m/m).

Q = 43 m³/sb = 6 my = 1.7 mz = 1.5n = 0.012
S = m/m
23.Pumps & pump powerMedium
PQ = 60 L/sH = 20 m

A pump with an efficiency of 75% delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 20 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 60 L/sH = 20 mη = 75%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 75 L/sΔz = 16 mL = 150 m, D = 200 mm, f = 0.022, ΣK = 8

A pump moves 75 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 16 m higher. The pipe is 150 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 82%. Find the shaft power Pshaft in kW.

Q = 75 L/sΔz = 16 mL = 150 mD = 200 mmf = 0.022ΣK = 8η = 82%
Pshaft = kW
25.Time value of moneyMedium
years0123…9PV = ?€6 000+2%+2%…r = 4%

A property is expected to earn net rent of €6 000 next year. The rent is expected to grow by 2% per year forever. The required return is 4% per year. Find the value PV of the property today.

C1 = €6 000g = 2%r = 4%
PV = €
26.Time value of moneyHard
months0123…96€200€200€200FV = ?

You save €200 at the end of every month for 8 years. The account pays 3.6% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €2003.6% / 12N = 96
FV = €
27.NPV & IRRMedium
years01234−75 00017 00024 00018 00023 000

An investment of €75 000 gives these cash flows at the end of years 1 to 4: €17 000, €24 000, €18 000, €23 000. The cost of capital is 6%. Find the net present value NPV.

r = 6%CF0 = −75 000CF1 = 17 000CF2 = 24 000CF3 = 18 000CF4 = 23 000
NPV = €
28.NPV & IRRHard
years012−50 00031 00024 000

A project costs €50 000 and returns €31 000, €24 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −50 000CF1 = 31 000CF2 = 24 000
IRR = %
29.Normal distributionMedium
242.75260.25P = ?

The bag weights are normally distributed with mean 250 g and standard deviation 5 g. What fraction lies between 242.75 and 260.25 g? Give P as a decimal.

μ = 250σ = 5x1 = 242.75x2 = 260.25
P =
30.Normal distributionHard
35455565758595pointsbottom 5%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Drag the cut-off so the shaded bottom 5% is to the left of it. Find the cut-off x.

μ = 65 pointsσ = 10 points5%
x = points

3Solutions

1.Beam support reactions

Answer: RA = 21.88 kN

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

P1​ = 25 kNP2​ = 25 kNABRA​RB​2 m0.5 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·4 = 25·2 + 25·2.5
RB = 112.5/4 = 28.13 kN
ΣFy = 0: RA = 50 − 28.13 = 21.88 kN

Answer

RA = 21.88 kN
2.Beam support reactions

Answer: RA = 46.88 kN

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

w = 10 kN/mP = 40 kNABRA​RB​2 m3 m3 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 = 10·3 = 30 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·8 = 40·2 + 10·3·3.5
RB = 185/8 = 23.13 kN
ΣFy = 0: RA = 70 − 23.13 = 46.88 kN

Answer

RA = 46.88 kN
3.Truss: method of joints

Answer: FAB = −33.94 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.

ABBCACACB60 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 60·3 → Cy = 36 kN
ΣFy = 0: Ay = 60 − 36 = 24 kN

Joint A

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

sin α = 3/4.243 = 0.7071
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −24/0.7071 = −33.94 kN

Answer

FAB = −33.94 kN (compression)
4.Truss: method of joints

Answer: FAC = 8.75 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.

ABBCACACB15 kN5 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 15·6 + 5·3 → Cy = 13.13 kN
ΣFy = 0: Ay = 15 − 13.13 = 1.875 kN
ΣFx = 0: Ax = −5 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 = 3/3.606 = 0.8321, cos γ = 2/3.606 = 0.5547
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −13.13/0.8321 = −15.77 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−15.77)·0.5547 = 8.75 kN

Answer

FAC = 8.75 kN (tension)
5.Shear force & bending moment

Answer: D (x = 3 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 = 25 kN, R2 = 25 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 = 22.5, MC = 40, MD = 52.5 kN·m, ME = 40, MF = 22.5, MG = 0

Answer

Mark D: MD = 52.5 kN·m
6.Shear force & bending moment

Answer: E (x = 8 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 = 42 kN, R2 = 112 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 = 68, MC = 104, MD = −2, ME = −140 kN·m, MF = −70, MG = 0

Answer

Mark E: ME = −140 kN·m
7.Beam deflection

Answer: δB = 5.013 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, a = 1000 mm, L = 2000 mm
EI = 3.99 × 10¹² N·mm²

Deflection at the free end

Deflection at the load plus the slope at the load times the remaining length.

δP = Pa³/(3EI) = 2.005 mm
θP = Pa²/(2EI) = 0.003008 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 5.013 mm

Answer

δB = 5.013 mm
8.Beam deflection

Answer: RB = 9 kN

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

Remove the prop

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

δload = wL⁴/(8EI)

Compatibility at the prop

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

RB·L³/(3EI) = wL⁴/(8EI) → RB = 3wL/8 = 3·4·6/8 = 9 kN

Answer

RB = 9 kN
9.Column buckling

Answer: Pcr = 35.09 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 = 60·20³/12 = 40000 mm⁴

Effective length

KL = 0.5·3000 = 1500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·40000/1500² = 35092 N = 35.09 kN

Answer

Pcr = 35.09 kN
10.Column buckling

Answer: d = 47.66 mm

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Required critical load

Pcr = n·P = 3·85000 = 255000 N
KL = 0.7·2000 = 1400 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·255000·1400²/(π³·200000))^(1/4) = 47.66 mm

Answer

d = 47.66 mm

Check: the slenderness KL/r is 117.5, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: ȳ = 36.43 mm

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 rectangles

Take the base at full width and the two legs above it (height h − t), so nothing is counted twice.

base: A1 = 200·10 = 2000 mm², y1 = 5 mm
two legs: A2 = 2·10·110 = 2200 mm², y2 = 10 + 110/2 = 65 mm

Centroid

ȳ = (2000·5 + 2200·65)/4200 = 36.43 mm

Answer

ȳ = 36.43 mm
12.Centroid & second moment of area

Answer: σtop = 37.92 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 = 240·20 = 4800 mm², yf = 140 + 20/2 = 150 mm
web: Aw = 18·140 = 2520 mm², yw = 140/2 = 70 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4800·150 + 2520·70)/7320 = 122.5 mm

Parallel-axis theorem

flange: 240·20³/12 + 4800·(150 − 122.5)² = 3.801 × 10⁶ mm⁴
web: 18·140³/12 + 2520·(70 − 122.5)² = 1.105 × 10⁷ mm⁴
Ix = 3.801 × 10⁶ + 1.105 × 10⁷ = 1.485 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 160 − 122.5 = 37.54 mm
σ = M·y/I = 1.5 × 10⁷·37.54/1.485 × 10⁷ = 37.92 MPa

Answer

σtop = 37.92 MPa
13.Effective stress in soil

Answer: σ′ = 128.1 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) = 16·1 + 20·11 = 236 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·11 = 107.9 kPa

Effective stress

σ′ = σ − u = 236 − 107.9 = 128.1 kPa

Answer

σ′ = 128.1 kPa
14.Effective stress in soil

Answer: σ′ = 71.85 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·2 + γsat,clay·2.5
σ = 15.5·2 + 20·2 + 18·2.5 = 116 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 = 116 − 44.15 = 71.85 kPa

Answer

σ′ = 71.85 kPa
15.Consolidation settlement

Answer: S = 86.57 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 = 95 + 200 = 295 kPa > 195 kPa

Settlement

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

S = 0.02·4/(1 + 0.95)·log₁₀(195/95) + 0.2·4/(1 + 0.95)·log₁₀(295/195)
S = 12.81 + 73.76 = 86.57 mm

Answer

S = 86.57 mm
16.Consolidation settlement

Answer: t = 24.63 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 = 0.197·10²/0.8 = 24.63 years

Answer

t = 24.63 years
17.Hydrostatic force

Answer: F = 119.6 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 = 2.5·1.5 = 3.75 m²
gated = 2 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.25·3.75 = 119.6 kN

Answer

F = 119.6 kN
18.Hydrostatic force

Answer: ycp = 5.349 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 + 2.5/2 = 5.25 m
A = H·b = 2.5·2 = 5 m²
gated = 4 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·5.25·5 = 226.6 kN

Centre of pressure

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

Ic = b·H³/12 = 2·2.5³/12 = 2.604 m⁴
ycp = yc + Ic/(yc·A) = 5.25 + 2.604/(5.25·5) = 5.349 m

Answer

ycp = 5.349 m
19.Pipe friction & head loss

Answer: Δp = 20.17 kPa

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.

Head loss

hf = f·(L/D)·V²/(2g) = 0.025·(100/0.075)·1.1²/(2·9.81) = 2.056 m

Pressure drop

The pipe is horizontal and the velocity does not change, so the energy equation reduces to Δp = ρ·g·hf.

Δp = ρ·g·hf = 1000·9.81·2.056 = 20167 Pa = 20.17 kPa

Answer

Δp = 20.17 kPa
20.Pipe friction & head loss

Answer: H = 0.9205 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 = 0.08/0.07069 = 1.132 m/s
V²/(2g) = 0.06529 m

Loss coefficients

f·L/D = 0.015·200/0.3 = 10
ΣK = 0.5 + 2·0.3 + 2 = 3.1

Energy equation

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

H = (1 + 10 + 3.1)·0.06529 = 0.9205 m

Answer

H = 0.9205 m
21.Open-channel flow (Manning)

Answer: Q = 3.163 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 + 1·0.6)·0.6 = 3.36 m²
P = b + 2y·√(1 + z²) = 5 + 2·0.6·√(1 + 1²) = 6.697 m
R = A/P = 0.5017 m

Velocity

V = (1/0.015)·0.50172/3·0.00051/2 = 0.9412 m/s

Flow rate

Q = A·V = 3.36·0.9412 = 3.163 m³/s

Answer

Q = 3.163 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0009902 m/m

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

Geometry

A = (b + z·y)·y = (6 + 1.5·1.7)·1.7 = 14.54 m²
P = b + 2y·√(1 + z²) = 6 + 2·1.7·√(1 + 1.5²) = 12.13 m
R = A/P = 1.198 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.012·43/(14.54·1.128) = 0.03147
S = 0.03147² = 0.0009902

Answer

S = 0.0009902

That is a fall of 0.9902 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 15.7 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 = 1000·9.81·0.06·20 = 11.77 kW

Shaft power

Pshaft = Ph/η = 11.77/0.75 = 15.7 kW

Answer

Pshaft = 15.7 kW
24.Pumps & pump power

Answer: Pshaft = 20.74 kW

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

Velocity

V = Q/A = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (16.5 + 8)·0.2905 = 7.117 m

Pump head

H = Δz + hL = 16 + 7.117 = 23.12 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.075·23.12/0.82 = 20.74 kW

Answer

Pshaft = 20.74 kW
25.Time value of money

Answer: PV = 300000 €

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.

Growing perpetuity

PV = C1/(r − g) = 6 000/(0.04 − 0.02) = 6 000/0.02 = €300 000.00

Answer

PV = €300 000.00
26.Time value of money

Answer: FV = 22212 €

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 = 0.036000000000000004/12 = 0.003
N = 12·8 = 96

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 200·(1.333 − 1)/0.003 = €22 212.16

Answer

FV = €22 212.16

You paid in €19 200 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −4271 €

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 = 17 000/1.06 = 16 037.74
CF2/(1 + 0.06)2 = 24 000/1.124 = 21 359.91
CF3/(1 + 0.06)3 = 18 000/1.191 = 15 113.15
CF4/(1 + 0.06)4 = 23 000/1.262 = 18 218.15

Add them up

NPV = €−4 271.05

Answer

NPV = €−4 271.05

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

28.NPV & IRR

Answer: IRR = 6.901 %

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%) = 1 292.52
NPV(10%) = −1 983.47

Narrow down

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

IRR ≈ 5 + 5·1 292.52/(1 292.52 − (−1 983.47)) = 6.973%
exact: NPV(6.901%) = 0 → IRR = 6.901%

Answer

IRR = 6.901%
29.Normal distribution

Answer: P = 0.9063

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 = (242.75 − 250)/5 = −1.45
z₂ = (260.25 − 250)/5 = 2.05

Area between

P = Φ(2.05) − Φ(−1.45) = 0.9798 − 0.07353 = 0.9063

Answer

P = 0.9063
30.Normal distribution

Answer: x = 48.6 points

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) = 0.05

z from the table

z ≈ −1.64

Back to the original units

x = 65 − 1.64·10 = 48.6 points

Answer

x = 48.6 points

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