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​ = 15 kNP2​ = 45 kNABRA​ = ?RB​2.5 m0.5 m1 m

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

L = 4 mP1 = 15 kN at 2.5 mP2 = 45 kN at 3 m
RA = kN
2.Beam support reactionsHard
w = 6 kN/mP = 45 kNABRA​RB​ = ?2 m1 m3 m

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

L = 6 mP = 45 kN at 3 mw = 6 kN/m from 2 to 6 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB25 kN8 m6 m4 m

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

span = 8 mheight = 4 mB is 6 m from Avertical load = 25 kN
FAC = kN
4.Truss: method of jointsHard
ABBCACACB30 kN20 kN4 m1 m2 m

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

span = 4 mheight = 2 mB is 1 m from Avertical load = 30 kNhorizontal load = 20 kN →
FBC = kN
5.Shear force & bending momentMedium
12 kN/m60 kNABCDEFG1 m1 m1 m1 m1 m1 m

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

60 kN @ 2 m12 kN/m, 0–6 m
  1. 1A (x = 0 m)
  2. 2B (x = 1 m)
  3. 3C (x = 2 m)
  4. 4D (x = 3 m)
  5. 5E (x = 4 m)
  6. 6F (x = 5 m)
  7. 7G (x = 6 m)
6.Shear force & bending momentHard
w = 10 kN/mABC4 m1.5 m

The beam rests on a pin at A and a roller at B and overhangs B by 1.5 m to the free end C. A uniformly distributed load w acts over the whole length A–C. Find the maximum sagging bending moment Mmax between the supports.

L = 5.5 mw = 10 kN/m from 0 to 5.5 msupports at x = 0 and x = 4 m
Mmax = kN·m
7.Beam deflectionMedium
P = 4 kNABδ6.5 m1.5 m

A simply supported beam carries a point load P at a = 6.5 m from support A. Find the deflection δP under the load.

P = 4 kNa = 6.5 mL = 8 mE = 70 GPa (aluminium)I = 8.5 × 10⁶ mm⁴
δP = mm
8.Beam deflectionHard
w = 10 kN/mAB3 m

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

L = 3 mw = 10 kN/m
RB = kN
9.Column bucklingMedium
PL = 2 m25 × 100 mmcross-section

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

L = 2 mE = 70 GPa (aluminium)b × h = 25 × 100 mm
Pcr = kN
10.Column bucklingHard
P = 130 kNL = 3 md = ?cross-section

A solid round column of length L made of steel is pinned at both ends. It must carry 130 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 130 kNn = 3L = 3 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
xD = 280d = 272dimensions in mm

A circular tube has outside diameter D = 280 mm and inside diameter d = 272 mm. Find its radius of gyration r about the horizontal centroidal axis.

D = 280 mmd = 272 mm
r = mm
12.Centroid & second moment of areaHard
130240163001614xdimensions in mm

A welded I-section has a top flange 130 × 16 mm, a web 300 mm high and 14 mm thick, and a bottom flange 240 × 16 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 130 × 16 mmweb: 14 × 300 mmbottom flange: 240 × 16 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 20.5 kN/m³9 mwater tableXz = 9 m

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

z = 9 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20.5 kN/m³
σ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 19 kN/m³5 mclayγsat​ = 18.5 kN/m³4 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 = 15.5 kN/m³sand: γsat = 19 kN/m³clay: γsat = 18.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 80 kPasandclayCc​ = 0.2, Cr​ = 0.06e0​ = 1.05σ′0​ = 120 kPaOCR = 32.5 mwater table

A 2.5 m thick overconsolidated clay layer has Cc = 0.2, Cr = 0.06 and e₀ = 1.05. At its mid-depth the effective vertical stress is 120 kPa and the overconsolidation ratio is OCR = 3. A new building adds 80 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2.5 mCc = 0.2Cr = 0.06e0 = 1.05σ′0 = 120 kPaOCR = 3Δσ = 80 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 7.5 m7.5 mimpervious rockwater table

In a laboratory oedometer test, a clay specimen 19 mm thick, drained at the top and bottom, reaches 50% consolidation in 8 min. In the field the same clay forms a layer 7.5 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 = 8 minH = 7.5 mfield: single drainage
t = days
17.Hydrostatic forceMedium
gated = 4 mH = 3 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 3 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 1 mH = 1.5 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of seawater, with its top edge 1 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1 mH = 1.5 mb = 1.5 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 25 L/sD = 100 mmL = 50 mf = 0.015

Water flows at 25 L/s through a pipe 50 m long with an inside diameter of 100 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the friction head loss hf.

Q = 25 L/sL = 50 mD = 100 mmf = 0.015g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2Δz = ?L = 300 m, D = 300 mm, f = 0.0222× bend (K = 0.3)

Two open reservoirs are joined by a pipe 300 m long with an inside diameter of 300 mm and a Darcy friction factor f = 0.022. The minor losses are a square-edged entrance (K = 0.5), 2 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 100 L/s?

Q = 100 L/sL = 300 mD = 300 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 2Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 5.5 my = 0.5 m3 : 1n = 0.015, S = 0.0015

A trapezoidal brickwork channel has a bottom width of 5.5 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 0.5 m deep. Manning n = 0.015 and the bed slope is S = 0.0015. Find the flow rate Q in m³/s.

b = 5.5 my = 0.5 mz = 3n = 0.015S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2 my = 0.6 m3 : 1n = 0.022, Q = 3.5 m³/s

A trapezoidal clean earth channel with a bottom width of 2 m and side slopes of 3:1 (horizontal:vertical) must carry 3.5 m³/s in uniform flow at a depth of 0.6 m. Manning n = 0.022. Find the required bed slope S (in m/m).

Q = 3.5 m³/sb = 2 my = 0.6 mz = 3n = 0.022
S = m/m
23.Pumps & pump powerMedium
PQ = 20 L/sH = 76 m

In a test, a pump delivers 20 L/s of water (ρ = 1000 kg/m³) against a head of 76 m while its shaft takes 19.1 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 20 L/sH = 76 mPshaft = 19.1 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 15 L/sΔz = 5 mL = 100 m, D = 100 mm, f = 0.015, ΣK = 8

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 5 m higher. The pipe is 100 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 70%. Find the shaft power Pshaft in kW.

Q = 15 L/sΔz = 5 mL = 100 mD = 100 mmf = 0.015ΣK = 8η = 70%
Pshaft = kW
25.Time value of moneyMedium
years01234567PV = ?€25 000

You need €25 000 in 7 years. An account pays 4% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €25 0004% / 12n = 7
PV = €
26.Time value of moneyHard
months0123…120€100€100€100FV = ?

You save €100 at the end of every month for 10 years. The account pays 5.4% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €1005.4% / 12N = 120
FV = €
27.NPV & IRRMedium
years0123…9−250 00030 000+1%+1%…r = 12%, NPV = ?

A project costs €250 000 today. It generates €30 000 at the end of the first year, and the cash flow then grows by 1% per year forever. The cost of capital is 12%. Find the net present value NPV.

C0 = €250 000CF1 = €30 000g = 1%r = 12%
NPV = €
28.NPV & IRRHard
years0123456−50 00010 000+4%+4%+4%+4%+4%r = 12%, NPV = ?

A project costs €50 000 today. Its cash flow is €10 000 at the end of year 1 and grows by 4% per year until the last cash flow at the end of year 6. The cost of capital is 12%. Find the net present value NPV.

C0 = €50 000CF1 = €10 000g = 4%n = 6r = 12%
NPV = €
29.Normal distributionMedium
76118P = ?

The IQ scores are normally distributed with mean 100 points and standard deviation 15 points. What fraction lies between 76 and 118 points? Give P as a decimal.

μ = 100σ = 15x1 = 76x2 = 118
P =
30.Normal distributionHard
μ = 500x = ?95%

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. Find the value x below which 95% of them lie (the 95th percentile).

μ = 500σ = 40P = 95%
x = h

3Solutions

1.Beam support reactions

Answer: RA = 16.88 kN

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

P1​ = 15 kNP2​ = 45 kNABRA​RB​2.5 m0.5 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·4 = 15·2.5 + 45·3
RB = 172.5/4 = 43.13 kN
ΣFy = 0: RA = 60 − 43.13 = 16.88 kN

Answer

RA = 16.88 kN
2.Beam support reactions

Answer: RB = 38.5 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 = 6 kN/mP = 45 kNABRA​RB​2 m1 m3 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 6·4 = 24 kN, acting at x̄ = 4 m
ΣMA = 0: RB·6 = 45·3 + 6·4·4
RB = 231/6 = 38.5 kN
ΣFy = 0: RA = 69 − 38.5 = 30.5 kN

Answer

RB = 38.5 kN
3.Truss: method of joints

Answer: FAC = 9.375 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 25·6 → Cy = 18.75 kN
ΣFy = 0: Ay = 25 − 18.75 = 6.25 kN

Joint C

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

sin γ = 4/4.472 = 0.8944, cos γ = 2/4.472 = 0.4472
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −18.75/0.8944 = −20.96 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−20.96)·0.4472 = 9.375 kN

Answer

FAC = 9.375 kN (tension)
4.Truss: method of joints

Answer: FBC = −31.55 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.

ABBCACACB30 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·4 = 30·1 + 20·2 → Cy = 17.5 kN
ΣFy = 0: Ay = 30 − 17.5 = 12.5 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 = 2/3.606 = 0.5547, cos γ = 3/3.606 = 0.8321
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −17.5/0.5547 = −31.55 kN

Answer

FBC = −31.55 kN (compression)
5.Shear force & bending moment

Answer: C (x = 2 m)

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

Support reactions

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

R1 = 76 kN, R2 = 56 kN

Bending moment at every mark

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

MA = 0, MB = 70, MC = 128 kN·m, MD = 114, ME = 88, MF = 50, MG = 0

Answer

Mark C: MC = 128 kN·m
6.Shear force & bending moment

Answer: Mmax = 14.77 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, including the load on the overhang.

UDL resultant: W = w·ℓ = 10·5.5 = 55 kN, acting at x̄ = 2.75 m
ΣMA = 0: RB·4 = 10·5.5·2.75
RB = 151.3/4 = 37.81 kN
ΣFy = 0: RA = 55 − 37.81 = 17.19 kN

Zero shear

RA − w·x0 = 0 → x0 = 17.19/10 = 1.719 m

Maximum sagging moment

Mmax = RA·x0 − w·x0²/2 = RA²/(2w) = 17.19²/(2·10) = 14.77 kN·m

Answer

Mmax = 14.77 kN·m
7.Beam deflection

Answer: δP = 26.63 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 = 4000 N, a = 6500 mm, b = 1500 mm, L = 8000 mm
EI = 5.95 × 10¹¹ N·mm²

Deflection under the load

δP = Pa²b²/(3EIL) = 4000·6500²·1500²/(3·5.95 × 10¹¹·8000) = 26.63 mm

Answer

δP = 26.63 mm
8.Beam deflection

Answer: RB = 11.25 kN

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

Remove the prop

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

δload = wL⁴/(8EI)

Compatibility at the prop

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

RB·L³/(3EI) = wL⁴/(8EI) → RB = 3wL/8 = 3·10·3/8 = 11.25 kN

Answer

RB = 11.25 kN
9.Column buckling

Answer: Pcr = 5.622 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 = 100·25³/12 = 130208 mm⁴

Effective length

KL = 2·2000 = 4000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·130208/4000² = 5622 N = 5.622 kN

Answer

Pcr = 5.622 kN
10.Column buckling

Answer: d = 77.58 mm

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

Required critical load

Pcr = n·P = 3·130000 = 390000 N
KL = 1·3000 = 3000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·390000·3000²/(π³·200000))^(1/4) = 77.58 mm

Answer

d = 77.58 mm

Check: the slenderness KL/r is 154.7, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: r = 97.59 mm

Second moment of area: for a rectangle about its own centroidal axis I = bh³/12, and about its base bh³/3 (parallel-axis theorem I = Ic + A·d²). A hole is handled by subtracting its I, as long as both parts share the same axis. The elastic section modulus is S = I/c, where c is the distance to the extreme fibre. The radius of gyration r = √(I/A) is the distance at which the whole area would give the same I; it is used in column buckling.

Net area and second moment of area

A = π(D² − d²)/4 = 3468 mm²
I = π(D⁴ − d⁴)/64 = 3.303 × 10⁷ mm⁴

Radius of gyration

r = √(I/A) = √(3.303 × 10⁷/3468) = 97.59 mm

Answer

r = 97.59 mm
12.Centroid & second moment of area

Answer: Ix = 171.8 × 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 three rectangles

Measure every y from the bottom edge.

top flange: A = 2080 mm², y = 324 mm
web: A = 4200 mm², y = 166 mm
bottom flange: A = 3840 mm², y = 8 mm

Centroid

ȳ = (2080·324 + 4200·166 + 3840·8)/10120 = 138.5 mm

Parallel-axis theorem

top flange: 130·16³/12 + 2080·185.5² = 7.16 × 10⁷ mm⁴
web: 14·300³/12 + 4200·27.48² = 3.467 × 10⁷ mm⁴
bottom flange: 240·16³/12 + 3840·130.5² = 6.55 × 10⁷ mm⁴
Ix = 7.16 × 10⁷ + 3.467 × 10⁷ + 6.55 × 10⁷
Ix = 1.718 × 10⁸ mm⁴ = 171.8 × 10⁶ mm⁴

Answer

Ix = 171.8 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ = 180 kPa

Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).

Total stress

Add the weight of each soil band above X. Above the water table use the dry unit weight, below it the saturated one.

σ = γd·zw + γsat·(z − zw) = 16·1 + 20.5·8 = 180 kPa

Answer

σ = 180 kPa
14.Effective stress in soil

Answer: σ′ = 82.26 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·2 + γsat,clay·2
σ = 15.5·3 + 19·2 + 18.5·2 = 121.5 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 = 121.5 − 39.24 = 82.26 kPa

Answer

σ′ = 82.26 kPa
15.Consolidation settlement

Answer: S = 16.23 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.

Preconsolidation pressure

σ′p = OCR·σ′0 = 3·120 = 360 kPa

Compare with the preconsolidation pressure

σ′f = 120 + 80 = 200 kPa ≤ 360 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.06·2.5/(1 + 1.05)·log₁₀(200/120) = 16.23 mm

Answer

S = 16.23 mm
16.Consolidation settlement

Answer: t = 3463 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 = 7.5 m

Scale the time

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

tfield = 8·(7.5/0.0095)² = 4.986 × 10⁶ min
tfield = 4.986 × 10⁶/1440 = 3463 days

Answer

t = 3463 days
17.Hydrostatic force

Answer: F = 242.8 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 = 4 + 3/2 = 5.5 m
A = H·b = 3·1.5 = 4.5 m²
gated = 4 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·5.5·4.5 = 242.8 kN

Answer

F = 242.8 kN
18.Hydrostatic force

Answer: F = 39.59 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 + 1.5/2 = 1.75 m
A = H·b = 1.5·1.5 = 2.25 m²
gated = 1 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·1.75·2.25 = 39.59 kN

Answer

F = 39.59 kN
19.Pipe friction & head loss

Answer: hf = 3.873 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·0.1²/4 = 0.007854 m²
V = Q/A = 0.025/0.007854 = 3.183 m/s

Velocity head

V²/(2g) = 3.183²/(2·9.81) = 0.5164 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.015·(50/0.1)·3.183²/(2·9.81) = 3.873 m

Answer

hf = 3.873 m
20.Pipe friction & head loss

Answer: Δz = 2.662 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 = 0.1/0.07069 = 1.415 m/s
V²/(2g) = 0.102 m

Loss coefficients

f·L/D = 0.022·300/0.3 = 22
ΣK = 0.5 + 2·0.3 + 2 + 1.0 = 4.1

Total head loss

hf = 22·0.102 = 2.244 m
hm = 4.1·0.102 = 0.4182 m
Δz = hf + hm = 2.662 m

Answer

Δz = 2.662 m
21.Open-channel flow (Manning)

Answer: Q = 4.939 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 = (5.5 + 3·0.5)·0.5 = 3.5 m²
P = b + 2y·√(1 + z²) = 5.5 + 2·0.5·√(1 + 3²) = 8.662 m
R = A/P = 0.4041 m

Velocity

V = (1/0.015)·0.40412/3·0.00151/2 = 1.411 m/s

Flow rate

Q = A·V = 3.5·1.411 = 4.939 m³/s

Answer

Q = 4.939 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003956 m/m

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

Geometry

A = (b + z·y)·y = (2 + 3·0.6)·0.6 = 2.28 m²
P = b + 2y·√(1 + z²) = 2 + 2·0.6·√(1 + 3²) = 5.795 m
R = A/P = 0.3935 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.022·3.5/(2.28·0.537) = 0.0629
S = 0.0629² = 0.003956

Answer

S = 0.003956

That is a fall of 3.956 m per kilometre.

23.Pumps & pump power

Answer: η = 78.07 %

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 = 1000·9.81·0.02·76 = 14.91 kW

Efficiency

η = Ph/Pshaft = 14.91/19.1 = 78.07%

Answer

η = 78.07%
24.Pumps & pump power

Answer: Pshaft = 1.95 kW

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

Velocity

V = Q/A = 0.015/0.007854 = 1.91 m/s
V²/(2g) = 0.1859 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (15 + 8)·0.1859 = 4.276 m

Pump head

H = Δz + hL = 5 + 4.276 = 9.276 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.015·9.276/0.7 = 1.95 kW

Answer

Pshaft = 1.95 kW
25.Time value of money

Answer: PV = 18903 €

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 = 0.04/12 = 0.003333
N = 12·7 = 84

Present value

PV = FV/(1 + i)N = 25 000/1.323 = €18 903.39

Answer

PV = €18 903.39
26.Time value of money

Answer: FV = 15865 €

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 = 0.054000000000000006/12 = 0.0045
N = 12·10 = 120

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 100·(1.714 − 1)/0.0045 = €15 865.10

Answer

FV = €15 865.10

You paid in €12 000 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = 22727 €

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.

Value of the cash flows

PV = 30 000/(0.12 − 0.01) = 272 727.27

NPV

NPV = 272 727.27 − 250 000 = €22 727.27

Answer

NPV = €22 727.27

NPV is positive, so the project earns more than the required return.

28.NPV & IRR

Answer: NPV = −5131 €

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 the growing annuity

((1.04)/(1.12))6 = 0.641
PV = 10 000/(0.12 − 0.04)·(1 − 0.641) = 44 868.75

NPV

NPV = 44 868.75 − 50 000 = −€5 131.25

Answer

NPV = −€5 131.25

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

29.Normal distribution

Answer: P = 0.8301

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 = (76 − 100)/15 = −1.6
z₂ = (118 − 100)/15 = 1.2

Area between

P = Φ(1.2) − Φ(−1.6) = 0.8849 − 0.0548 = 0.8301

Answer

P = 0.8301
30.Normal distribution

Answer: x = 565.8 h

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 for the percentile

Φ(z) = 0.95 → z = 1.645

Back to x

x = 500 + 1.645·40 = 565.8 h

Answer

x = 565.8 h

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