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​ = 60 kNP2​ = 25 kNABRA​RB​ = ?1 m1 m6 m

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

L = 8 mP1 = 60 kN at 1 mP2 = 25 kN at 2 m
RB = kN
2.Beam support reactionsHard
w = 12 kN/mP = 35 kNABRA​ = ?RB​1 m2 m1 m

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

L = 4 mP = 35 kN at 3 mw = 12 kN/m from 1 to 4 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB60 kN8 m3 m2 m

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

span = 8 mheight = 2 mB is 3 m from Avertical load = 60 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB20 kN20 kN5 m4 m2 m

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

span = 5 mheight = 2 mB is 4 m from Avertical load = 20 kNhorizontal load = 20 kN →
FAC = kN
5.Shear force & bending momentMedium
M0​ = 40 kN·mAB1 m7 m

The simply supported beam carries a clockwise couple M0 = 40 kN·m at x = 1 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 = 40 kN·m clockwise, at 1 m
Mx = kN·m
6.Shear force & bending momentHard
w = 6 kN/mAB9 m1 m

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

L = 10 mw = 6 kN/m from 0 to 9 m
Mmax = kN·m
7.Beam deflectionMedium
w = 10 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 = 10 kN/mL = 3 mE = 70 GPa (aluminium)I = 12 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 2 kN/mδL = 3 m

A simply supported beam carries a uniformly distributed load w. Its deflection may not exceed span/360. Find the smallest second moment of area Ireq that meets this limit.

w = 2 kN/mL = 3 mE = 200 GPa (steel)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 2.5 md = 60 mmcross-section

A column of length L made of aluminium is fixed at the base and pinned at the top. Using Euler’s formula, find its critical buckling load Pcr.

L = 2.5 mE = 70 GPa (aluminium)d = 60 mm
Pcr = kN
10.Column bucklingHard
PL = 4 md = 50 mmcross-section

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

L = 4 mE = 70 GPa (aluminium)d = 50 mm
σcr = MPa
11.Centroid & second moment of areaMedium
2801024020xdimensions in mm

Find the second moment of area Ix of the T-section about the horizontal axis x through its centroid.

bf = 280 mmtf = 10 mmtw = 20 mmhw = 240 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2402020014xM = 10 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 10 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 240 mmtf = 20 mmtw = 14 mmhw = 200 mmM = 10 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 19.5 kN/m³13 mwater tableXz = 9 m

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

z = 9 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 20 kN/m³3 mclayγsat​ = 17 kN/m³8 mwater tableXz = 7 m

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

z = 7 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20 kN/m³clay: γsat = 17 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 10 kPasandclayCc​ = 0.35, Cr​ = 0.03e0​ = 1σ′0​ = 110 kPaσ′p​ = 160 kPa5 mwater table

A 5 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.03 and e₀ = 1. At its mid-depth the effective vertical stress is 110 kPa and the preconsolidation pressure is 160 kPa. A new building adds 10 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 5 mCc = 0.35Cr = 0.03e0 = 1σ′0 = 110 kPaσ′p = 160 kPaΔσ = 10 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 6.5 m6.5 mimpervious rockwater table

In a laboratory oedometer test, a clay specimen 19 mm thick, drained at the top and bottom, reaches 50% consolidation in 5 min. In the field the same clay forms a layer 6.5 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 = 19 mmtlab = 5 minH = 6.5 mfield: single drainage
t = days
17.Hydrostatic forceMedium
gated = 0.5 mH = 3 m

A vertical rectangular gate 3 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 = 3 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 1 mH = 3 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of glycerin, with its top edge 1 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 1 mH = 3 mb = 1.5 mρ = 1260 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 1.6 m/sD = 75 mmL = 1000 mf = 0.028

Water (ρ = 1000 kg/m³) flows at 1.6 m/s through a horizontal pipe, 1000 m long, with an inside diameter of 75 mm. Use the Darcy friction factor f = 0.028 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1.6 m/sL = 1000 mD = 75 mmf = 0.028ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 2Δz = ?L = 400 m, D = 200 mm, f = 0.0154× bend (K = 0.3)

Two open reservoirs are joined by a pipe 400 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.015. The minor losses are a square-edged entrance (K = 0.5), 4 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 75 L/s?

Q = 75 L/sL = 400 mD = 200 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 2Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 6 my = 2 m1 : 1n = 0.014, S = 0.004

A trapezoidal unfinished concrete channel has a bottom width of 6 m and side slopes of 1:1 (horizontal:vertical). Water flows uniformly 2 m deep. Manning n = 0.014 and the bed slope is S = 0.004. Find the flow rate Q in m³/s.

b = 6 my = 2 mz = 1n = 0.014S = 0.004
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 450 mmn = 0.013, V = 0.6 m/s

A concrete sewer with an inside diameter of 450 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.6 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 450 mmn = 0.013V = 0.6 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 100 L/sH = 54 m

A pump delivers 100 L/s of water (ρ = 1000 kg/m³) against a head of 54 m. The pump efficiency is 70% and the electric motor driving it has an efficiency of 92%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 100 L/sH = 54 mηpump = 70%ηmotor = 92%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
150 kPa (gauge)PQ = 50 L/sΔz = 8 mL = 300 m, D = 200 mm, f = 0.022, ΣK = 5

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 300 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 = 5 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 150 kPa. Find the head H the pump must add.

Q = 50 L/sΔz = 8 mL = 300 mD = 200 mmf = 0.022ΣK = 5ptank = 150 kPa
H = m
25.Time value of moneyMedium
years01234€10 000FV = ?

You invest €10 000 at 6% per year with continuous compounding. Find the value FV after 4 years.

PV = €10 000r = 6%t = 4
FV = €
26.Time value of moneyHard
years0123…29€5 000€5 000€5 000FV = ?

You deposit €5 000 at the start of every year for 29 years, the first deposit today. The account pays 6% per year. How much is in the account at the end of year 29? Find FV.

A = €5 000i = 6%n = 29
FV = €
27.NPV & IRRMedium
years0123−30 00011 00011 00010 000

An investment of €30 000 gives these cash flows at the end of years 1 to 3: €11 000, €11 000, €10 000. The cost of capital is 12%. Find the net present value NPV.

r = 12%CF0 = −30 000CF1 = 11 000CF2 = 11 000CF3 = 10 000
NPV = €
28.NPV & IRRHard
years0123−25 00014 00016 00013 000

A project costs €25 000 and returns €14 000, €16 000, €13 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −25 000CF1 = 14 000CF2 = 16 000CF3 = 13 000
IRR = %
29.Normal distributionMedium
765 kg819 kgT = X₁ + … + X₉?

The masses of passengers with luggage are independent and normal with mean 85 kg and standard deviation 12 kg. Find the probability P that the total mass of 9 of them is below 819 kg. Round z to two decimals.

μ = 85 kgσ = 12 kgn = 9< 819 kg
P =
30.Normal distributionHard
235240245250255260265gbottom 60%

The bag weights are normally distributed with mean 250 g and standard deviation 5 g. Drag the cut-off so the shaded bottom 60% is to the left of it. Find the cut-off x.

μ = 250 gσ = 5 g60%
x = g

3Solutions

1.Beam support reactions

Answer: RB = 13.75 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​ = 60 kNP2​ = 25 kNABRA​RB​1 m1 m6 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 = 60·1 + 25·2
RB = 110/8 = 13.75 kN
ΣFy = 0: RA = 85 − 13.75 = 71.25 kN

Answer

RB = 13.75 kN
2.Beam support reactions

Answer: RA = 22.25 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 = 12 kN/mP = 35 kNABRA​RB​1 m2 m1 m

Free-body diagram

Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.

Equilibrium

Moments about A, counter-clockwise positive. Then vertical force balance.

UDL resultant: W = w·ℓ = 12·3 = 36 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·4 = 35·3 + 12·3·2.5
RB = 195/4 = 48.75 kN
ΣFy = 0: RA = 71 − 48.75 = 22.25 kN

Answer

RA = 22.25 kN
3.Truss: method of joints

Answer: FAB = −67.6 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·8 = 60·3 → Cy = 22.5 kN
ΣFy = 0: Ay = 60 − 22.5 = 37.5 kN

Joint A

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

sin α = 2/3.606 = 0.5547
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −37.5/0.5547 = −67.6 kN

Answer

FAB = −67.6 kN (compression)
4.Truss: method of joints

Answer: FAC = 12 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.

ABBCACACB20 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 20·4 + 20·2 → Cy = 24 kN
ΣFy = 0: Ay = 20 − 24 = −4 kN
ΣFx = 0: Ax = −20 kN

Joint C

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

sin γ = 2/2.236 = 0.8944, cos γ = 1/2.236 = 0.4472
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −24/0.8944 = −26.83 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−26.83)·0.4472 = 12 kN

Answer

FAC = 12 kN (tension)
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 = 40/8 = 5 kN (upward)
RA = −RB = −5 kN (downward)

Cut just left of the couple

The left part contains only RA.

Mx = RA·a = −5·1 = −5 kN·m

Answer

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

Answer: Mmax = 73.51 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut. Maximum moment: since dM/dx = V, the bending moment has its peak where the shear force passes through zero, either at a point load or inside a distributed load.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 6·9 = 54 kN, acting at x̄ = 4.5 m
ΣMA = 0: RB·10 = 6·9·4.5
RB = 243/10 = 24.3 kN
ΣFy = 0: RA = 54 − 24.3 = 29.7 kN

Zero shear

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

RA − w·(x0 − 0) = 0
x0 = 0 + 29.7/6 = 4.95 m

Maximum moment

Mmax = RA·x0 − w·(x0 − 0)²/2 = 29.7·4.95 − 6·4.95²/2 = 73.51 kN·m

Answer

Mmax = 73.51 kN·m
7.Beam deflection

Answer: δmax = 12.56 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 = 10 N/mm, L = 3000 mm
EI = 8.4 × 10¹¹ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·10·3000⁴/(384·8.4 × 10¹¹) = 12.56 mm

Answer

δmax = 12.56 mm
8.Beam deflection

Answer: Ireq = 1.266 × 10⁶ mm⁴

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).

Deflection limit

δallow = L/360 = 3000/360 = 8.333 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·2·3000⁴/(384·200000·8.333) = 1.266 × 10⁶ mm⁴
Ireq = 1.266 × 10⁶ mm⁴

Answer

Ireq = 1.266 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 143.5 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·60⁴/64 = 636173 mm⁴

Effective length

KL = 0.7·2500 = 1750 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·636173/1750² = 143515 N = 143.5 kN

Answer

Pcr = 143.5 kN
10.Column buckling

Answer: σcr = 6.747 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·50⁴/64 = 306796 mm⁴

Radius of gyration and slenderness

A = 1963 mm²
r = √(I/A) = √(306796/1963) = 12.5 mm
KL = 1·4000 = 4000 mm
KL/r = 4000/12.5 = 320

Critical stress

σcr = π²E/(KL/r)² = π²·70000/320² = 6.747 MPa

Answer

σcr = 6.747 MPa
11.Centroid & second moment of area

Answer: Ix = 50.69 × 10⁶ mm⁴

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

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 280·10 = 2800 mm², yf = 240 + 10/2 = 245 mm
web: Aw = 20·240 = 4800 mm², yw = 240/2 = 120 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2800·245 + 4800·120)/7600 = 166.1 mm

Parallel-axis theorem

flange: 280·10³/12 + 2800·(245 − 166.1)² = 1.747 × 10⁷ mm⁴
web: 20·240³/12 + 4800·(120 − 166.1)² = 3.322 × 10⁷ mm⁴
Ix = 1.747 × 10⁷ + 3.322 × 10⁷ = 5.069 × 10⁷ mm⁴ = 50.69 × 10⁶ mm⁴

Answer

Ix = 50.69 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 16.36 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 = 200 + 20/2 = 210 mm
web: Aw = 14·200 = 2800 mm², yw = 200/2 = 100 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4800·210 + 2800·100)/7600 = 169.5 mm

Parallel-axis theorem

flange: 240·20³/12 + 4800·(210 − 169.5)² = 8.043 × 10⁶ mm⁴
web: 14·200³/12 + 2800·(100 − 169.5)² = 2.285 × 10⁷ mm⁴
Ix = 8.043 × 10⁶ + 2.285 × 10⁷ = 3.089 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 220 − 169.5 = 50.53 mm
σ = M·y/I = 1 × 10⁷·50.53/3.089 × 10⁷ = 16.36 MPa

Answer

σtop = 16.36 MPa
13.Effective stress in soil

Answer: σ′ = 93.52 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 + 19.5·8 = 172 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·8 = 78.48 kPa

Effective stress

σ′ = σ − u = 172 − 78.48 = 93.52 kPa

Answer

σ′ = 93.52 kPa
14.Effective stress in soil

Answer: u = 49.05 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) = 9.81·5 = 49.05 kPa

Answer

u = 49.05 kPa
15.Consolidation settlement

Answer: S = 2.834 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 = 110 + 10 = 120 kPa ≤ 160 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.03·5/(1 + 1)·log₁₀(120/110) = 2.834 mm

Answer

S = 2.834 mm
16.Consolidation settlement

Answer: t = 1626 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 = 19/2 = 9.5 mm = 0.0095 m
Hdr,field = 6.5 m

Scale the time

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

tfield = 5·(6.5/0.0095)² = 2.341 × 10⁶ min
tfield = 2.341 × 10⁶/1440 = 1626 days

Answer

t = 1626 days
17.Hydrostatic force

Answer: F = 176.6 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 = 0.5 + 3/2 = 2 m
A = H·b = 3·3 = 9 m²
gated = 0.5 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2·9 = 176.6 kN

Answer

F = 176.6 kN
18.Hydrostatic force

Answer: ycp = 2.8 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 = 1 + 3/2 = 2.5 m
A = H·b = 3·1.5 = 4.5 m²
gated = 1 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·2.5·4.5 = 139.1 kN

Centre of pressure

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

Ic = b·H³/12 = 1.5·3³/12 = 3.375 m⁴
ycp = yc + Ic/(yc·A) = 2.5 + 3.375/(2.5·4.5) = 2.8 m

Answer

ycp = 2.8 m
19.Pipe friction & head loss

Answer: Δp = 477.9 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) = 0.028·(1000/0.075)·1.6²/(2·9.81) = 48.71 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 = 1000·9.81·48.71 = 477867 Pa = 477.9 kPa

Answer

Δp = 477.9 kPa
20.Pipe friction & head loss

Answer: Δz = 10.08 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 = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m

Loss coefficients

f·L/D = 0.015·400/0.2 = 30
ΣK = 0.5 + 4·0.3 + 2 + 1.0 = 4.7

Total head loss

hf = 30·0.2905 = 8.715 m
hm = 4.7·0.2905 = 1.365 m
Δz = hf + hm = 10.08 m

Answer

Δz = 10.08 m
21.Open-channel flow (Manning)

Answer: Q = 89.27 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 + 1·2)·2 = 16 m²
P = b + 2y·√(1 + z²) = 6 + 2·2·√(1 + 1²) = 11.66 m
R = A/P = 1.373 m

Velocity

V = (1/0.014)·1.3732/3·0.0041/2 = 5.579 m/s

Flow rate

Q = A·V = 16·5.579 = 89.27 m³/s

Answer

Q = 89.27 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.00112 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 = 0.45/4 = 0.1125 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.6/0.233)² = 0.00112

Answer

S = 0.00112

That is a fall of 1.12 m per kilometre.

23.Pumps & pump power

Answer: Pel = 82.26 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 = 1000·9.81·0.1·54 = 52.97 kW

Shaft power

Pshaft = 52.97/0.7 = 75.68 kW

Electrical power

Pel = 75.68/0.92 = 82.26 kW

Answer

Pel = 82.26 kW
24.Pumps & pump power

Answer: H = 28.2 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) = (33 + 5)·0.1291 = 4.906 m

Pressure head

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

Pump head

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

H = Δz + p/(ρ·g) + hL = 8 + 15.29 + 4.906 = 28.2 m

Answer

H = 28.2 m
25.Time value of money

Answer: FV = 12712 €

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.

Exponent

r·t = 0.06·4 = 0.24
e0.24 = 1.271

Future value

FV = 10 000·1.271 = €12 712.49

Answer

FV = €12 712.49
26.Time value of money

Answer: FV = 390291 €

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.

Ordinary annuity factor

((1 + 0.06)29 − 1)/0.06 = 73.64

Annuity due

Each deposit is invested one year longer.

FV = 5 000·73.64·1.06 = €390 290.93

Answer

FV = €390 290.93
27.NPV & IRR

Answer: NPV = −4292 €

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 = −30 000
CF1/(1 + 0.12)1 = 11 000/1.12 = 9 821.43
CF2/(1 + 0.12)2 = 11 000/1.254 = 8 769.13
CF3/(1 + 0.12)3 = 10 000/1.405 = 7 117.80

Add them up

NPV = €−4 291.64

Answer

NPV = €−4 291.64

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

28.NPV & IRR

Answer: IRR = 33.29 %

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

Bracket the IRR

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

NPV(30%) = 1 153.85
NPV(35%) = −566.73

Narrow down

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

IRR ≈ 30 + 5·1 153.85/(1 153.85 − (−566.73)) = 33.35%
exact: NPV(33.29%) = 0 → IRR = 33.29%

Answer

IRR = 33.29%
29.Normal distribution

Answer: P = 0.9332

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 total

μT = 765 kg, σT = 12·√9 = 36 kg

Standardise

z = (819 − 765)/36 = 1.5

Probability

P = Φ(1.5) = 0.9332

Answer

P = 0.9332
30.Normal distribution

Answer: x = 251.3 g

From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.

Area to the left

Φ(z) = 0.6

z from the table

z ≈ 0.25

Back to the original units

x = 250 + 0.25·5 = 251.3 g

Answer

x = 251.3 g

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