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​ = 35 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 RA.

L = 8 mP1 = 40 kN at 1 mP2 = 35 kN at 7 m
RA = kN
2.Beam support reactionsHard
w = 8 kN/mP = 10 kNABRA​RB​ = ?2.5 m0.5 m1 m2 m

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

L = 6 mP = 10 kN at 2.5 mw = 8 kN/m from 3 to 4 m
RB = kN
3.Truss: method of jointsMedium
ABCDEFGH25 kN15 kN40 kN40 kN4 × 3 m4 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

B: 25 kN ↓C: 15 kN ↓D: 40 kN ↓F: 40 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member FC
  13. 13member HC
4.Truss: method of jointsHard
ABBCACACB25 kN15 kN6 m1 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 1 m from Avertical load = 25 kNhorizontal load = 15 kN ←
FAC = kN
5.Shear force & bending momentMedium
M0​ = 10 kN·mAB4 m4 m

The simply supported beam carries a clockwise couple M0 = 10 kN·m at x = 4 m from A, and no other load. Find the bending moment Mx just to the left of the couple. Use sagging moments positive and upward shear on the left face positive.

L = 8 mM0 = 10 kN·m clockwise, at 4 m
Mx = kN·m
6.Shear force & bending momentHard
w = 8 kN/mP = 40 kNABsection1 m1 m2 m

Find the bending moment Mx at the section x = 1 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mP = 40 kN at 2 mw = 8 kN/m from 0 to 4 mx = 1 m
Mx = kN·m
7.Beam deflectionMedium
w = 15 kN/mδL = 3 m

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

w = 15 kN/mL = 3 mE = 70 GPa (aluminium)I = 84 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 2 kN/mP = 23 kNδL = 2.5 m

A simply supported beam carries a uniformly distributed load w and a point load P at midspan. Using superposition, find the midspan deflection δmax.

P = 23 kNw = 2 kN/mL = 2.5 mE = 11 GPa (timber)I = 84 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 3 m20 × 40 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 = 3 mE = 70 GPa (aluminium)b × h = 20 × 40 mm
Pcr = kN
10.Column bucklingHard
PL = 6 md = 40 mmcross-section

A column of length L made of aluminium is fixed at both ends. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 6 mE = 70 GPa (aluminium)d = 40 mm
σcr = MPa
11.Centroid & second moment of areaMedium
200 mm200 mm130 mmØ30xIx​ = ?

A 200 mm × 200 mm plate has a circular hole of diameter 30 mm on its vertical centre line, with its centre 130 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 200 mmh = 200 mmd = 30 mmhole centre: y = 130 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
180101408xhogging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 60 MPa in tension and 100 MPa in compression. Find the largest hogging bending moment Mallow the beam can carry (give its size).

bf = 180 mmtf = 10 mmtw = 8 mmhw = 140 mmσt,allow = 60 MPaσc,allow = 100 MPa
Mallow = kN·m
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 18.5 kN/m³9 mwater tableXz = 7 m

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

z = 7 mzw = 4 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 18.5 kN/m³
σ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 20.5 kN/m³6 mclayγsat​ = 17 kN/m³5 mwater tableXz = 8.5 m

For the soil profile shown, find the pore water pressure u at point X.

z = 8.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 17 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 180 kPasandclayCc​ = 0.5, Cr​ = 0.03e0​ = 0.9σ′0​ = 115 kPaσ′p​ = 185 kPa5 mwater table

A 5 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.03 and e₀ = 0.9. At its mid-depth the effective vertical stress is 115 kPa and the preconsolidation pressure is 185 kPa. A new building adds 180 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 5 mCc = 0.5Cr = 0.03e0 = 0.9σ′0 = 115 kPaσ′p = 185 kPaΔσ = 180 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 7 m7 mimpervious rockwater table

In a laboratory oedometer test, a clay specimen 25 mm thick, drained at the top and bottom, reaches 50% consolidation in 15 min. In the field the same clay forms a layer 7 m thick. It lies on impervious rock, with sand above it, so water drains out only at the top. How many days t does the field layer take to reach 50% consolidation?

hlab = 25 mmtlab = 15 minH = 7 mfield: single drainage
t = days
17.Hydrostatic forceMedium
gated = 2.5 mH = 2.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 2.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2.5 mH = 2.5 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2 mH = 3 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of glycerin, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 3 mb = 3 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 4 L/sD = 50 mmL = 200 mf = 0.03

Water flows at 4 L/s through a pipe 200 m long with an inside diameter of 50 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

Q = 4 L/sL = 200 mD = 50 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5Δz = ?L = 400 m, D = 300 mm, f = 0.0182× bend (K = 0.3)

Two open reservoirs are joined by a pipe 400 m long with an inside diameter of 300 mm and a Darcy friction factor f = 0.018. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each), a valve (K = 5) 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 75 L/s?

Q = 75 L/sL = 400 mD = 300 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 5 my = 0.9 m3 : 1n = 0.022, S = 0.001

A trapezoidal clean earth channel has a bottom width of 5 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 0.9 m deep. Manning n = 0.022 and the bed slope is S = 0.001. Find the flow rate Q in m³/s.

b = 5 my = 0.9 mz = 3n = 0.022S = 0.001
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 1 my = 1.5 mn = 0.025, Q = 2 m³/s

A rectangular gravel channel 1 m wide must carry 2 m³/s in uniform flow at a depth of 1.5 m. Manning n = 0.025. Find the required bed slope S (in m/m).

Q = 2 m³/sb = 1 my = 1.5 mn = 0.025
S = m/m
23.Pumps & pump powerMedium
PQ = 40 L/sH = 40 m

A pump delivers 40 L/s of water (ρ = 1000 kg/m³) against a head of 40 m. The pump efficiency is 65% and the electric motor driving it has an efficiency of 94%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 40 L/sH = 40 mηpump = 65%ηmotor = 94%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
300 kPa (gauge)PQ = 15 L/sΔz = 12 mL = 100 m, D = 100 mm, f = 0.02, ΣK = 6

A pump moves 15 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 100 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 300 kPa. Find the head H the pump must add.

Q = 15 L/sΔz = 12 mL = 100 mD = 100 mmf = 0.02ΣK = 6ptank = 300 kPa
H = m
25.Time value of moneyMedium
periods0123411 + EAR = ?22% / 4

A credit card charges a nominal interest rate of 22% per year, compounded quarterly. Find the effective annual rate EAR in percent.

r = 22%m = 4
EAR = %
26.Time value of moneyHard
months0123…36€15 000AAAA5.4% / 12, I = ?

A loan of €15 000 is repaid with equal monthly payments over 3 years at 5.4% per year, compounded monthly. How much interest I is paid in total over the life of the loan?

P = €15 0005.4% / 12N = 36
I = €
27.NPV & IRRMedium
years012345€80 000€4 000€4 000€4 000€4 000€4 000r = 5%, EAC = ?

A machine costs €80 000 today, lasts 5 years and costs €4 000 per year to run (paid at the end of each year). The cost of capital is 5%. Find its equivalent annual cost EAC.

C0 = €80 000M = €4 000n = 5r = 5%
EAC = €
28.NPV & IRRHard
years012−50 00025 50029 000

A project costs €50 000 and returns €25 500, €29 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −50 000CF1 = 25 500CF2 = 29 000
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area to the right of z = 0.2236

Drag z so that the shaded area under the standard normal curve, to the right of z, is 0.2236. Find z to two decimals.

A = 0.2236
z =
30.Normal distributionHard
0.05 mm0D − d?

Hole diameters D are normal with mean 25.05 mm and standard deviation 0.02 mm. Shaft diameters d are independent and normal with mean 25 mm and standard deviation 0.015 mm. A randomly chosen shaft fits when D − d > 0. Find the probability P that it fits. Round z to two decimals.

hole: μ = 25.05 mm, σ = 0.02 mmshaft: μ = 25 mm, σ = 0.015 mm
P =

3Solutions

1.Beam support reactions

Answer: RA = 39.38 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​ = 35 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 = 40·1 + 35·7
RB = 285/8 = 35.63 kN
ΣFy = 0: RA = 75 − 35.63 = 39.38 kN

Answer

RA = 39.38 kN
2.Beam support reactions

Answer: RB = 8.833 kN

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

w = 8 kN/mP = 10 kNABRA​RB​2.5 m0.5 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 = 8·1 = 8 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·6 = 10·2.5 + 8·1·3.5
RB = 53/6 = 8.833 kN
ΣFy = 0: RA = 18 − 8.833 = 9.167 kN

Answer

RB = 8.833 kN
3.Truss: method of joints

Answer: member CG

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint G

FG and GH lie on one straight line and the joint carries no load. Balancing forces across that line leaves only CG.

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

Solving all joints gives these member forces (T = tension, C = compression).

AB: 49.69 kN (T), BC: 49.69 kN (T), CD: 40.31 kN (T), DE: 40.31 kN (T), FG: 50.63 kN (C), GH: 50.63 kN (C), AF: 82.81 kN (C), HE: 67.19 kN (C), BF: 25 kN (T), CG: 0, DH: 40 kN (T), FC: 1.563 kN (T), HC: 17.19 kN (T)

Answer

Zero-force member: CG
4.Truss: method of joints

Answer: FAC = −2.083 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.

ABBCACACB25 kN15 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 25·1 − 15·2 → Cy = −0.8333 kN
ΣFy = 0: Ay = 25 − −0.8333 = 25.83 kN
ΣFx = 0: Ax = 15 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 = 2/5.385 = 0.3714, cos γ = 5/5.385 = 0.9285
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −−0.8333/0.3714 = 2.244 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(2.244)·0.9285 = −2.083 kN

Answer

FAC = −2.083 kN (compression)
5.Shear force & bending moment

Answer: Mx = −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. An applied couple makes the bending moment diagram jump by the size of the couple.

Support reactions

Moments about A, counter-clockwise positive: RB·L − M0 = 0. Vertical balance: RA + RB = 0.

RB = M0/L = 10/8 = 1.25 kN (upward)
RA = −RB = −1.25 kN (downward)

Cut just left of the couple

The left part contains only RA.

Mx = RA·a = −1.25·4 = −5 kN·m

Answer

Mx = −5 kN·m
6.Shear force & bending moment

Answer: Mx = 32 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 = 8·4 = 32 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 40·2 + 8·4·2
RB = 144/4 = 36 kN
ΣFy = 0: RA = 72 − 36 = 36 kN
w = 8 kN/mP = 40 kNABRA​ = 36RB​ = 36section1 m1 m2 m

Cut at x = 1 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 = 36·1 − 8·1·0.5 = 32 kN·m

Answer

Mx = 32 kN·m
7.Beam deflection

Answer: δmax = 2.691 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 = 15 N/mm, L = 3000 mm
EI = 5.88 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·15·3000⁴/(384·5.88 × 10¹²) = 2.691 mm

Answer

δmax = 2.691 mm
8.Beam deflection

Answer: δmax = 9.204 mm

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

Consistent units

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

P = 23000 N, w = 2 N/mm, L = 2500 mm, EI = 9.24 × 10¹¹ N·mm²

Each load on its own

δP = PL³/(48EI) = 23000·2500³/(48·9.24 × 10¹¹) = 8.103 mm
δw = 5wL⁴/(384EI) = 5·2·2500⁴/(384·9.24 × 10¹¹) = 1.101 mm

Add them

δmax = 8.103 + 1.101 = 9.204 mm

Answer

δmax = 9.204 mm
9.Column buckling

Answer: Pcr = 8.188 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 = 40·20³/12 = 26667 mm⁴

Effective length

KL = 0.5·3000 = 1500 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·26667/1500² = 8188 N = 8.188 kN

Answer

Pcr = 8.188 kN
10.Column buckling

Answer: σcr = 7.676 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·40⁴/64 = 125664 mm⁴

Radius of gyration and slenderness

A = 1257 mm²
r = √(I/A) = √(125664/1257) = 10 mm
KL = 0.5·6000 = 3000 mm
KL/r = 3000/10 = 300

Critical stress

σcr = π²E/(KL/r)² = π²·70000/300² = 7.676 MPa

Answer

σcr = 7.676 MPa
11.Centroid & second moment of area

Answer: Ix = 132.6 × 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 = (40000·100 − 706.9·130)/(40000 − 706.9) = 99.46 mm

Full plate about ȳ

200·200³/12 + 40000·0.5397² = 133.3 × 10⁶ mm⁴

Hole about ȳ

π·30⁴/64 + 706.9·30.54² = 0.699 × 10⁶ mm⁴

Subtract

Ix = 132.6 × 10⁶ mm⁴

Answer

Ix = 132.6 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 4.928 kN·m

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

Centroid

ȳ = (1800·145 + 1120·70)/2920 = 116.2 mm
top edge: c = 150 − 116.2 = 33.77 mm

Second moment of area

I = 180·10³/12 + 1800·28.77² + 8·140³/12 + 1120·46.23² = 5.728 × 10⁶ mm⁴

Moment allowed by each edge

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

top edge: M = 60·5.728 × 10⁶/33.77 = 10.18 kN·m
bottom edge: M = 100·5.728 × 10⁶/116.2 = 4.928 kN·m

Governing value

Mallow = min = 4.928 kN·m (bottom edge)

Answer

Mallow = 4.928 kN·m
13.Effective stress in soil

Answer: σ = 115.5 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) = 15·4 + 18.5·3 = 115.5 kPa

Answer

σ = 115.5 kPa
14.Effective stress in soil

Answer: u = 63.77 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).

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·6.5 = 63.77 kPa

Answer

u = 63.77 kPa
15.Consolidation settlement

Answer: S = 282.9 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 = 115 + 180 = 295 kPa > 185 kPa

Settlement

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

S = 0.03·5/(1 + 0.9)·log₁₀(185/115) + 0.5·5/(1 + 0.9)·log₁₀(295/185)
S = 16.3 + 266.6 = 282.9 mm

Answer

S = 282.9 mm
16.Consolidation settlement

Answer: t = 3267 days

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 paths

Hdr,lab = 25/2 = 12.5 mm = 0.0125 m
Hdr,field = 7 m

Scale the time

t = Tv·Hdr²/cv with the same T_v and cv in the lab and the field.

tfield = 15·(7/0.0125)² = 4.704 × 10⁶ min
tfield = 4.704 × 10⁶/1440 = 3267 days

Answer

t = 3267 days
17.Hydrostatic force

Answer: F = 183.9 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 + 2.5/2 = 3.75 m
A = H·b = 2.5·2 = 5 m²
gated = 2.5 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.75·5 = 183.9 kN

Answer

F = 183.9 kN
18.Hydrostatic force

Answer: F = 389.4 kN

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

Centroid depth and area

yc = d + H/2 = 2 + 3/2 = 3.5 m
A = H·b = 3·3 = 9 m²
gated = 2 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·3.5·9 = 389.4 kN

Answer

F = 389.4 kN
19.Pipe friction & head loss

Answer: hf = 25.38 m

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

Mean velocity

A = π·0.05²/4 = 0.001963 m²
V = Q/A = 0.004/0.001963 = 2.037 m/s

Velocity head

V²/(2g) = 2.037²/(2·9.81) = 0.2115 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(200/0.05)·2.037²/(2·9.81) = 25.38 m

Answer

hf = 25.38 m
20.Pipe friction & head loss

Answer: Δz = 1.785 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 = 0.075/0.07069 = 1.061 m/s
V²/(2g) = 0.05738 m

Loss coefficients

f·L/D = 0.018·400/0.3 = 24
ΣK = 0.5 + 2·0.3 + 5 + 1.0 = 7.1

Total head loss

hf = 24·0.05738 = 1.377 m
hm = 7.1·0.05738 = 0.4074 m
Δz = hf + hm = 1.785 m

Answer

Δz = 1.785 m
21.Open-channel flow (Manning)

Answer: Q = 7.46 m³/s

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

Geometry

A = (b + z·y)·y = (5 + 3·0.9)·0.9 = 6.93 m²
P = b + 2y·√(1 + z²) = 5 + 2·0.9·√(1 + 3²) = 10.69 m
R = A/P = 0.6481 m

Velocity

V = (1/0.022)·0.64812/3·0.0011/2 = 1.077 m/s

Flow rate

Q = A·V = 6.93·1.077 = 7.46 m³/s

Answer

Q = 7.46 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.004109 m/m

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

Geometry

A = b·y = 1·1.5 = 1.5 m²
P = b + 2y = 1 + 2·1.5 = 4 m
R = A/P = 0.375 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.025·2/(1.5·0.52) = 0.0641
S = 0.0641² = 0.004109

Answer

S = 0.004109

That is a fall of 4.109 m per kilometre.

23.Pumps & pump power

Answer: Pel = 25.69 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 = 1000·9.81·0.04·40 = 15.7 kW

Shaft power

Pshaft = 15.7/0.65 = 24.15 kW

Electrical power

Pel = 24.15/0.94 = 25.69 kW

Answer

Pel = 25.69 kW
24.Pumps & pump power

Answer: H = 47.41 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 = 0.015/0.007854 = 1.91 m/s
V²/(2g) = 0.1859 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (20 + 6)·0.1859 = 4.834 m

Pressure head

p/(ρ·g) = 300000/(1000·9.81) = 30.58 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 12 + 30.58 + 4.834 = 47.41 m

Answer

H = 47.41 m
25.Time value of money

Answer: EAR = 23.88 %

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 = 0.22/4 = 0.055

Compound over one year

EAR = (1 + 0.055)4 − 1 = 1.239 − 1 = 23.88%

Answer

EAR = 23.88%

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

26.Time value of money

Answer: I = 1281 €

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 = 0.0045, N = 36
A = 15 000·0.0045/(1 − (1 + 0.0045)−36) = €452.26

Total interest

I = N·A − P = 36·452.3 − 15 000 = €1 281.44

Answer

I = €1 281.44
27.NPV & IRR

Answer: EAC = 22478 €

Equivalent annual cost: spread the present value of all costs over the life as an equal yearly amount (an annuity): EAC = PV·r/(1 − (1 + r)⁻ⁿ). It lets you compare machines with different lives.

Annuity factor

(1 − 1.05−5)/0.05 = 4.329

Annualised purchase price

80 000/4.329 = 18 477.98

EAC

EAC = 18 477.98 + 4 000 = €22 477.98

Answer

EAC = €22 477.98
28.NPV & IRR

Answer: IRR = 5.813 %

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%) = 589.57
NPV(10%) = −2 851.24

Narrow down

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

IRR ≈ 5 + 5·589.57/(589.57 − (−2 851.24)) = 5.857%
exact: NPV(5.813%) = 0 → IRR = 5.813%

Answer

IRR = 5.813%
29.Normal distribution

Answer: z = 0.76

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 − 0.2236 = 0.7764

Read the z-table backwards

Find 0.7764 inside the table and read off z.

z = 0.76

Answer

z = 0.76
30.Normal distribution

Answer: P = 0.9772

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 = 25.05 − 25 = 0.05 mm, σ = 0.025 mm

Standardise

z = (0 − 0.05)/0.025 = −2

Probability

P = 1 − Φ(−2) = 0.9772

Answer

P = 0.9772

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