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​ = 55 kNP2​ = 50 kNABRA​ = ?RB​1 m1 m2 m

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

L = 4 mP1 = 55 kN at 1 mP2 = 50 kN at 2 m
RA = kN
2.Beam support reactionsHard
w = 8 kN/mP = 25 kNQ = 60 kNADCMA​ = ?1.5 m0.5 m2 m2 m

A compound beam is fixed to the wall at A, has an internal hinge at C (2 m from A) and rests on a roller at D (6 m from A). It carries a point load P at 4 m from A, a uniformly distributed load w on the whole part CD and a point load Q at 1.5 m from A. Find the magnitude of the reaction moment MA at the wall.

AC = 2 mAD = 6 mP = 25 kN at 4 mw = 8 kN/m from 2 to 6 mQ = 60 kN at 1.5 m
MA = kN·m
3.Truss: method of jointsMedium
ABBCACACB20 kN4 m1 m3 m

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

span = 4 mheight = 3 mB is 1 m from Avertical load = 20 kN
FAB = kN
4.Truss: method of jointsHard
ABCDEFGH25 kN20 kN10 kN15 kN4 × 3 m3 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 ↓G: 20 kN ↓H: 10 kN ↓H: 15 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
5.Shear force & bending momentMedium
P1​ = 80 kNP2​ = 10 kNABC4 m4 m2 m

The beam rests on a pin at A and a roller at B and overhangs B by 2 m to the free end C. It carries a point load P1 between the supports and a point load P2 at C. Find the bending moment MB at support B. Use sagging moments positive and upward shear on the left face positive.

L = 10 mP1 = 80 kN at 4 mP2 = 10 kN at 10 msupports at x = 0 and x = 8 m
MB = kN·m
6.Shear force & bending momentHard
w = 3 kN/mP = 45 kNABsection2.5 m2.5 m

Find the bending moment Mx at the section x = 2.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mP = 45 kN at 2.5 mw = 3 kN/m from 0 to 5 mx = 2.5 m
Mx = kN·m
7.Beam deflectionMedium
w = 6 kN/mδL = 6 m

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

w = 6 kN/mL = 6 mE = 70 GPa (aluminium)I = 84 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 4 kN/mP = 29 kNδL = 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 = 29 kNw = 4 kN/mL = 5 mE = 200 GPa (steel)I = 8.5 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 3 md = 25 mmcross-section

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

L = 3 mE = 200 GPa (steel)d = 25 mm
Pcr = kN
10.Column bucklingHard
PL = 2.5 md = 40 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 = 2.5 mE = 70 GPa (aluminium)d = 40 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1401514020xdimensions in mm

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

bf = 140 mmtf = 15 mmtw = 20 mmhw = 140 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1002512020xM = 25 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 25 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 100 mmtf = 25 mmtw = 20 mmhw = 120 mmM = 25 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 20 kN/m³9 mwater tableXz = 9 m

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

z = 9 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 20.5 kN/m³4 mclayγsat​ = 17.5 kN/m³6 mwater tableXz = 7 m

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

z = 7 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 17.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 30 kPasandclayCc​ = 0.2, Cr​ = 0.05e0​ = 0.65σ′0​ = 95 kPaσ′p​ = 155 kPa4.5 mwater table

A 4.5 m thick overconsolidated clay layer has Cc = 0.2, Cr = 0.05 and e₀ = 0.65. At its mid-depth the effective vertical stress is 95 kPa and the preconsolidation pressure is 155 kPa. A new building adds 30 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 4.5 mCc = 0.2Cr = 0.05e0 = 0.65σ′0 = 95 kPaσ′p = 155 kPaΔσ = 30 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 5 mcv​ = 2 m²/year5 msandwater table

A clay layer 5 m thick has a coefficient of consolidation cv = 2 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 60% average consolidation the time factor is Tv = 0.287. How many years t does the layer take to reach 60% consolidation?

H = 5 mcv = 2 m²/yearU = 60%Tv = 0.287double drainage
t = years
17.Hydrostatic forceMedium
gated = 0.5 mH = 1.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.

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

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of seawater, with its top edge 1.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1.5 mH = 2 mb = 1.5 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 60 L/sD = 250 mmL = 100 mf = 0.03

Water flows at 60 L/s through a pipe 100 m long with an inside diameter of 250 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

Q = 60 L/sL = 100 mD = 250 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2free outletH = ?L = 300 m, D = 300 mm, f = 0.0224× bend (K = 0.3)

A pipe 300 m long with an inside diameter of 300 mm (Darcy friction factor f = 0.022) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each) and a valve (K = 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 = 300 mD = 300 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 2
H = m
21.Open-channel flow (Manning)Medium
D = 300 mmn = 0.013, S = 0.0005

A concrete storm sewer with an inside diameter of 300 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.0005. Find the flow rate Q in m³/s.

D = 300 mmn = 0.013S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2.5 my = 1.5 mn = 0.014, Q = 11 m³/s

A rectangular unfinished concrete channel 2.5 m wide must carry 11 m³/s in uniform flow at a depth of 1.5 m. Manning n = 0.014. Find the required bed slope S (in m/m).

Q = 11 m³/sb = 2.5 my = 1.5 mn = 0.014
S = m/m
23.Pumps & pump powerMedium
PQ = 50 L/sH = 44 m

A pump with an efficiency of 60% delivers 50 L/s of water (ρ = 1000 kg/m³) against a head of 44 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 50 L/sH = 44 mη = 60%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 60 L/sΔz = 10 mL = 100 m, D = 200 mm, f = 0.018, ΣK = 4

A pump moves 60 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 10 m higher. The pipe is 100 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 4 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 60 L/sΔz = 10 mL = 100 mD = 200 mmf = 0.018ΣK = 4
H = m
25.Time value of moneyMedium
years01234PV = ?€5 000

You need €5 000 in 4 years. An account pays 3% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €5 0003% / 12n = 4
PV = €
26.Time value of moneyHard
months0123…192A?AA€30 000

You want €30 000 in 16 years. You save the same amount at the end of every month in an account paying 4.8% per year, compounded monthly. Find the monthly deposit A.

FV = €30 0004.8% / 12N = 192
A = €
27.NPV & IRRMedium
years0123−75 00027 00032 00026 000

An investment of €75 000 gives these cash flows at the end of years 1 to 3: €27 000, €32 000, €26 000. The cost of capital is 12%. Find the net present value NPV.

r = 12%CF0 = −75 000CF1 = 27 000CF2 = 32 000CF3 = 26 000
NPV = €
28.NPV & IRRHard
years012−40 00026 50022 000

A project costs €40 000 and returns €26 500, €22 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 26 500CF2 = 22 000
IRR = %
29.Normal distributionMedium
57.577.5P = ?

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. What fraction lies between 57.5 and 77.5 points? Give P as a decimal.

μ = 65σ = 10x1 = 57.5x2 = 77.5
P =
30.Normal distributionHard
10 g0X − Y?

The mass X of a product from line 1 and Y from line 2 are independent and normal: X has mean 500 g and standard deviation 8 g, Y has mean 490 g and standard deviation 6 g. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 500 g, σX = 8 gμY = 490 g, σY = 6 g
P =

3Solutions

1.Beam support reactions

Answer: RA = 66.25 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.

P1​ = 55 kNP2​ = 50 kNABRA​RB​1 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.

ΣMA = 0: RB·4 = 55·1 + 50·2
RB = 155/4 = 38.75 kN
ΣFy = 0: RA = 105 − 38.75 = 66.25 kN

Answer

RA = 66.25 kN
2.Beam support reactions

Answer: MA = 147 kN·m

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Replace each distributed load by its resultant (its area) acting at the centroid of the load diagram, and take moments about a support to remove that support’s reaction from the equation. An internal hinge cannot carry a bending moment, which gives one extra equation: the moment about the hinge of the forces on either side is zero.

Part CD

The hinge has no moment, so moments about C on CD alone must balance.

W = 8·4 = 32 kN at 2 m from C
ΣMC = 0: RD·4 = 25·2 + 32·2
RD = 28.5 kN
VC = 57 − 28.5 = 28.5 kN

Part AC

The hinge force VC acts downward on AC (equal and opposite to its action on CD).

RA = 60 + 28.5 = 88.5 kN
MA = 60·1.5 + 28.5·2 = 147 kN·m

Answer

MA = 147 kN·m
3.Truss: method of joints

Answer: FAB = −15.81 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·4 = 20·1 → Cy = 5 kN
ΣFy = 0: Ay = 20 − 5 = 15 kN

Joint A

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

sin α = 3/3.162 = 0.9487
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −15/0.9487 = −15.81 kN

Answer

FAB = −15.81 kN (compression)
4.Truss: method of joints

Answer: member DH

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 D

CD and DE lie on one straight line and the joint carries no load. Balancing forces across that line leaves only DH.

ΣF⊥ = 0 → FDH = 0

Check with the method of joints

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

AB: 20 kN (T), BC: 20 kN (T), CD: 20 kN (T), DE: 20 kN (T), FG: 45 kN (C), GH: 45 kN (C), AF: 49.5 kN (C), HE: 28.28 kN (C), BF: 25 kN (T), CG: 20 kN (C), DH: 0, FC: 14.14 kN (T), HC: 14.14 kN (T)

Answer

Zero-force member: DH
5.Shear force & bending moment

Answer: MB = −20 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. The overhang load also acts about A.

ΣMA = 0: RB·8 = 80·4 + 10·10
RB = 420/8 = 52.5 kN
ΣFy = 0: RA = 90 − 52.5 = 37.5 kN

Cut at B and keep the overhang

Only P2 acts on the overhang, with lever arm a. It bends the beam upward over the support (hogging).

MB = −P2·a = −10·2 = −20 kN·m

Answer

MB = −20 kN·m
6.Shear force & bending moment

Answer: Mx = 65.63 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 3·5 = 15 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 45·2.5 + 3·5·2.5
RB = 150/5 = 30 kN
ΣFy = 0: RA = 60 − 30 = 30 kN
w = 3 kN/mP = 45 kNABRA​ = 30RB​ = 30section2.5 m2.5 m

Cut at x = 2.5 m and keep the left part

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

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 30·2.5 − 3·2.5·1.25 = 65.63 kN·m

Answer

Mx = 65.63 kN·m
7.Beam deflection

Answer: δmax = 17.22 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 = 6 N/mm, L = 6000 mm
EI = 5.88 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·6·6000⁴/(384·5.88 × 10¹²) = 17.22 mm

Answer

δmax = 17.22 mm
8.Beam deflection

Answer: δmax = 63.57 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 = 29000 N, w = 4 N/mm, L = 5000 mm, EI = 1.7 × 10¹² N·mm²

Each load on its own

δP = PL³/(48EI) = 29000·5000³/(48·1.7 × 10¹²) = 44.42 mm
δw = 5wL⁴/(384EI) = 5·4·5000⁴/(384·1.7 × 10¹²) = 19.15 mm

Add them

δmax = 44.42 + 19.15 = 63.57 mm

Answer

δmax = 63.57 mm
9.Column buckling

Answer: Pcr = 16.82 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·25⁴/64 = 19175 mm⁴

Effective length

KL = 0.5·3000 = 1500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·19175/1500² = 16822 N = 16.82 kN

Answer

Pcr = 16.82 kN
10.Column buckling

Answer: σcr = 11.05 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 = 1·2500 = 2500 mm
KL/r = 2500/10 = 250

Critical stress

σcr = π²E/(KL/r)² = π²·70000/250² = 11.05 MPa

Answer

σcr = 11.05 MPa
11.Centroid & second moment of area

Answer: Ix = 11.82 × 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 = 140·15 = 2100 mm², yf = 140 + 15/2 = 147.5 mm
web: Aw = 20·140 = 2800 mm², yw = 140/2 = 70 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2100·147.5 + 2800·70)/4900 = 103.2 mm

Parallel-axis theorem

flange: 140·15³/12 + 2100·(147.5 − 103.2)² = 4.158 × 10⁶ mm⁴
web: 20·140³/12 + 2800·(70 − 103.2)² = 7.662 × 10⁶ mm⁴
Ix = 4.158 × 10⁶ + 7.662 × 10⁶ = 1.182 × 10⁷ mm⁴ = 11.82 × 10⁶ mm⁴

Answer

Ix = 11.82 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 127.1 MPa

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

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 100·25 = 2500 mm², yf = 120 + 25/2 = 132.5 mm
web: Aw = 20·120 = 2400 mm², yw = 120/2 = 60 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2500·132.5 + 2400·60)/4900 = 96.99 mm

Parallel-axis theorem

flange: 100·25³/12 + 2500·(132.5 − 96.99)² = 3.283 × 10⁶ mm⁴
web: 20·120³/12 + 2400·(60 − 96.99)² = 6.164 × 10⁶ mm⁴
Ix = 3.283 × 10⁶ + 6.164 × 10⁶ = 9.446 × 10⁶ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 145 − 96.99 = 48.01 mm
σ = M·y/I = 2.5 × 10⁷·48.01/9.446 × 10⁶ = 127.1 MPa

Answer

σtop = 127.1 MPa
13.Effective stress in soil

Answer: u = 58.86 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 = 58.86 kPa

Answer

u = 58.86 kPa
14.Effective stress in soil

Answer: σ′ = 81.76 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·3 + γsat,sand·1 + γsat,clay·3
σ = 16·3 + 20.5·1 + 17.5·3 = 121 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·4 = 39.24 kPa

Effective stress

σ′ = σ − u = 121 − 39.24 = 81.76 kPa

Answer

σ′ = 81.76 kPa
15.Consolidation settlement

Answer: S = 16.25 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 + 30 = 125 kPa ≤ 155 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·4.5/(1 + 0.65)·log₁₀(125/95) = 16.25 mm

Answer

S = 16.25 mm
16.Consolidation settlement

Answer: t = 0.8969 years

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

Drainage path

Hdr = H/2 = 5/2 = 2.5 m

Time

t = Tv·Hdr²/cv = 0.287·2.5²/2 = 0.8969 years

Answer

t = 0.8969 years
17.Hydrostatic force

Answer: F = 36.79 kN

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

Centroid depth and area

yc = d + H/2 = 0.5 + 1.5/2 = 1.25 m
A = H·b = 1.5·2 = 3 m²
gated = 0.5 mH = 1.5 mF

Resultant force

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

Answer

F = 36.79 kN
18.Hydrostatic force

Answer: F = 75.41 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 = 1.5 + 2/2 = 2.5 m
A = H·b = 2·1.5 = 3 m²
gated = 1.5 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·2.5·3 = 75.41 kN

Answer

F = 75.41 kN
19.Pipe friction & head loss

Answer: hf = 0.9138 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·0.25²/4 = 0.04909 m²
V = Q/A = 0.06/0.04909 = 1.222 m/s

Velocity head

V²/(2g) = 1.222²/(2·9.81) = 0.07615 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(100/0.25)·1.222²/(2·9.81) = 0.9138 m

Answer

hf = 0.9138 m
20.Pipe friction & head loss

Answer: H = 1.743 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 = 0.022·300/0.3 = 22
ΣK = 0.5 + 4·0.3 + 2 = 3.7

Energy equation

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

H = (1 + 22 + 3.7)·0.06529 = 1.743 m

Answer

H = 1.743 m
21.Open-channel flow (Manning)

Answer: Q = 0.02162 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 = 0.07069 m², R = D/4 = 0.075 m

Velocity

V = (1/0.013)·0.0752/3·0.00051/2 = 0.3059 m/s

Flow rate

Q = A·V = 0.07069·0.3059 = 0.02162 m³/s

Answer

Q = 0.02162 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.00281 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 = 2.5·1.5 = 3.75 m²
P = b + 2y = 2.5 + 2·1.5 = 5.5 m
R = A/P = 0.6818 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.014·11/(3.75·0.7747) = 0.05301
S = 0.05301² = 0.00281

Answer

S = 0.00281

That is a fall of 2.81 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 35.97 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 = 1000·9.81·0.05·44 = 21.58 kW

Shaft power

Pshaft = Ph/η = 21.58/0.6 = 35.97 kW

Answer

Pshaft = 35.97 kW
24.Pumps & pump power

Answer: H = 12.42 m

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

Velocity

V = Q/A = 0.06/0.03142 = 1.91 m/s
V²/(2g) = 0.1859 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (9 + 4)·0.1859 = 2.417 m

Pump head

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

H = Δz + hL = 10 + 2.417 = 12.42 m

Answer

H = 12.42 m
25.Time value of money

Answer: PV = 4435 €

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

Rate and number of periods

i = 0.03/12 = 0.0025
N = 12·4 = 48

Present value

PV = FV/(1 + i)N = 5 000/1.127 = €4 435.27

Answer

PV = €4 435.27
26.Time value of money

Answer: A = 104.2 €

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 = 0.048/12 = 0.004
N = 12·16 = 192

Deposit

A = FV·i/((1 + i)N − 1) = 30 000·0.004/(2.152 − 1) = €104.15

Answer

A = €104.15
27.NPV & IRR

Answer: NPV = −6876 €

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 + 0.12)1 = 27 000/1.12 = 24 107.14
CF2/(1 + 0.12)2 = 32 000/1.254 = 25 510.20
CF3/(1 + 0.12)3 = 26 000/1.405 = 18 506.29

Add them up

NPV = €−6 876.37

Answer

NPV = €−6 876.37

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

28.NPV & IRR

Answer: IRR = 14.35 %

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(10%) = 2 272.73
NPV(15%) = −321.36

Narrow down

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

IRR ≈ 10 + 5·2 272.73/(2 272.73 − (−321.36)) = 14.38%
exact: NPV(14.35%) = 0 → IRR = 14.35%

Answer

IRR = 14.35%
29.Normal distribution

Answer: P = 0.6677

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 = (57.5 − 65)/10 = −0.75
z₂ = (77.5 − 65)/10 = 1.25

Area between

P = Φ(1.25) − Φ(−0.75) = 0.8944 − 0.2266 = 0.6677

Answer

P = 0.6677
30.Normal distribution

Answer: P = 0.8413

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 = 500 − 490 = 10 g, σ = 10 g

Standardise

z = (0 − 10)/10 = −1

Probability

P = 1 − Φ(−1) = 0.8413

Answer

P = 0.8413

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