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.

New problemsBack to the course

In the print window, choose “Save as PDF” to keep a copy on your device.

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
P = 75 kNM = 60 kN·mABRA​ = ?1 m6 m1 m

The simply supported beam has a pin at A and a roller at B. It carries a point load P at 7 m from A and a counter-clockwise couple M at 1 m from A. Find the vertical reaction RA, taking upward as positive.

L = 8 mP = 75 kN at 7 mM = 60 kN·m (counter-clockwise) at 1 m
RA = kN
2.Beam support reactionsHard
w = 8 kN/mP = 60 kNABRA​ = ?RB​3 m4 m1 m2 m

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

L = 10 mP = 60 kN at 3 mw = 8 kN/m from 7 to 8 m
RA = kN
3.Truss: method of jointsMedium
ABCDEFGH10 kN35 kN10 kN4 × 4 m4 m

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

B: 10 kN ↓F: 35 kN ↓G: 10 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 BG
  13. 13member DG
4.Truss: method of jointsHard
ABBCACACB50 kN20 kN5 m1 m4 m

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

span = 5 mheight = 4 mB is 1 m from Avertical load = 50 kNhorizontal load = 20 kN ←
FBC = kN
5.Shear force & bending momentMedium
10 kN/m20 kNABCDEFG2 m2 m2 m2 m2 m2 m

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

20 kN @ 6 m10 kN/m, 2–8 m
  1. 1A (x = 0 m)
  2. 2B (x = 2 m)
  3. 3C (x = 4 m)
  4. 4D (x = 6 m)
  5. 5E (x = 8 m)
  6. 6F (x = 10 m)
  7. 7G (x = 12 m)
6.Shear force & bending momentHard
5 kN/m35 kN45 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.

35 kN @ 6 m45 kN @ 2 m5 kN/m, 0–4 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)
7.Beam deflectionMedium
P = 5 kNABδ1 m3 m

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

P = 5 kNa = 1 mL = 4 mE = 11 GPa (timber)I = 120 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
w = 4 kN/mP = 15 kNδL = 6 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 = 15 kNw = 4 kN/mL = 6 mE = 200 GPa (steel)I = 120 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 3 m40 × 80 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 = 3 mE = 70 GPa (aluminium)b × h = 40 × 80 mm
Pcr = kN
10.Column bucklingHard
P = 15 kNL = 3 md = ?cross-section

A solid round column of length L made of steel is fixed at both ends. It must carry 15 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 15 kNn = 2L = 3 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
30090t = 8xdimensions in mm

A channel section lies with its open side up: a base plate 300 mm wide with two upright legs, 90 mm high overall. Base and legs are all 8 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.

b = 300 mmh = 90 mmt = 8 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
3002016012xM = 30 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 30 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 300 mmtf = 20 mmtw = 12 mmhw = 160 mmM = 30 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 20.5 kN/m³14 mwater tableXz = 7 m

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

z = 7 mzw = 4 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 20 kN/m³6 mclayγsat​ = 17 kN/m³7 mwater tableXz = 9.5 m

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

z = 9.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 20 kN/m³clay: γsat = 17 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 45 kPasandclayCc​ = 0.3, Cr​ = 0.05e0​ = 0.6σ′0​ = 95 kPaσ′p​ = 195 kPa4 mwater table

A 4 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.05 and e₀ = 0.6. At its mid-depth the effective vertical stress is 95 kPa and the preconsolidation pressure is 195 kPa. A new building adds 45 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 4 mCc = 0.3Cr = 0.05e0 = 0.6σ′0 = 95 kPaσ′p = 195 kPaΔσ = 45 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 3 mcv​ = 2 m²/year3 mimpervious rockwater table

A clay layer 3 m thick has a coefficient of consolidation cv = 2 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 70% average consolidation the time factor is Tv = 0.403. How many years t does the layer take to reach 70% consolidation?

H = 3 mcv = 2 m²/yearU = 70%Tv = 0.403single drainage
t = years
17.Hydrostatic forceMedium
gated = 4 mH = 2 m

A vertical rectangular gate 3 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 = 2 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 3 mH = 1 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of glycerin, with its top edge 3 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 3 mH = 1 mb = 1 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 10 L/sD = 100 mmL = 200 mf = 0.022

Water flows at 10 L/s through a pipe 200 m long with an inside diameter of 100 mm. Use the Darcy friction factor f = 0.022 and g = 9.81 m/s². Find the friction head loss hf.

Q = 10 L/sL = 200 mD = 100 mmf = 0.022g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2free outletH = ?L = 100 m, D = 100 mm, f = 0.0254× bend (K = 0.3)

A pipe 100 m long with an inside diameter of 100 mm (Darcy friction factor f = 0.025) 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 10 L/s?

Q = 10 L/sL = 100 mD = 100 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 2
H = m
21.Open-channel flow (Manning)Medium
D = 750 mmn = 0.013, S = 0.0015

A concrete storm sewer with an inside diameter of 750 mm flows half full. Manning n = 0.013 and the slope is S = 0.0015. Find the flow rate Q in m³/s.

D = 750 mmn = 0.013S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 3.5 my = 0.9 m1.5 : 1n = 0.03, Q = 6 m³/s

A trapezoidal grass-lined earth channel with a bottom width of 3.5 m and side slopes of 1.5:1 (horizontal:vertical) must carry 6 m³/s in uniform flow at a depth of 0.9 m. Manning n = 0.03. Find the required bed slope S (in m/m).

Q = 6 m³/sb = 3.5 my = 0.9 mz = 1.5n = 0.03
S = m/m
23.Pumps & pump powerMedium
PQ = 20 L/sH = 54 m

A pump with an efficiency of 85% delivers 20 L/s of water (ρ = 1000 kg/m³) against a head of 54 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 20 L/sH = 54 mη = 85%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
100 kPa (gauge)PQ = 80 L/sΔz = 10 mL = 100 m, D = 200 mm, f = 0.018, ΣK = 2.5

A pump moves 80 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 = 2.5 (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 100 kPa. Find the head H the pump must add.

Q = 80 L/sΔz = 10 mL = 100 mD = 200 mmf = 0.018ΣK = 2.5ptank = 100 kPa
H = m
25.Time value of moneyMedium
years0123…20PV = ?€5 000€5 000€5 000€5 000

An annuity pays €5 000 at the end of each year for 20 years. The interest rate is 6% per year. Find the present value PV of the annuity.

A = €5 000i = 6%n = 20
PV = €
26.Time value of moneyHard
months01…288…360€250 000AB = ?A2.4% / 12

A mortgage of €250 000 is repaid with equal monthly payments over 30 years at 2.4% per year, compounded monthly. How much is still owed just after the payment at the end of year 24? Find the outstanding balance B.

P = €250 0002.4% / 12N = 360k = 288
B = €
27.NPV & IRRMedium
years01234−45 00012 00021 00013 00016 000

An investment of €45 000 gives these cash flows at the end of years 1 to 4: €12 000, €21 000, €13 000, €16 000. The cost of capital is 9%. Find the net present value NPV.

r = 9%CF0 = −45 000CF1 = 12 000CF2 = 21 000CF3 = 13 000CF4 = 16 000
NPV = €
28.NPV & IRRHard
years01234−50 00028 50028 00017 00026 000

A project costs €50 000 and returns €28 500, €28 000, €17 000, €26 000 at the end of years 1 to 4. Cash flows can be reinvested at the cost of capital of 8%. Find the modified internal rate of return MIRR in percent.

r = 8%CF0 = −50 000CF1 = 28 500CF2 = 28 000CF3 = 17 000CF4 = 26 000
MIRR = %
29.Normal distributionMedium
320 g318.3 gT = X₁ + … + X₈?

The masses of bolts are independent and normal with mean 40 g and standard deviation 1.2 g. Find the probability P that the total mass of 8 of them exceeds 318.3 g. Round z to two decimals.

μ = 40 gσ = 1.2 gn = 8> 318.3 g
P =
30.Normal distributionHard
μ = 250x = ?99%

The bag weights are normally distributed with mean 250 g and standard deviation 5 g. Find the value x below which 99% of them lie (the 99th percentile).

μ = 250σ = 5P = 99%
x = g

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. 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.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·8 − 75·7 + 60 = 0
RB = 465/8 = 58.13 kN

Vertical equilibrium

RA = 75 − 58.13 = 16.88 kN

Answer

RA = 16.88 kN

A negative reaction acts downward.

2.Beam support reactions

Answer: RA = 44 kN

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

w = 8 kN/mP = 60 kNABRA​RB​3 m4 m1 m2 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 8·1 = 8 kN, acting at x̄ = 7.5 m
ΣMA = 0: RB·10 = 60·3 + 8·1·7.5
RB = 240/10 = 24 kN
ΣFy = 0: RA = 68 − 24 = 44 kN

Answer

RA = 44 kN
3.Truss: method of joints

Answer: member CG

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

Joint C

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

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

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

AB: 38.75 kN (T), BC: 32.5 kN (T), CD: 32.5 kN (T), DE: 16.25 kN (T), FG: 38.75 kN (C), GH: 16.25 kN (C), AF: 54.8 kN (C), HE: 22.98 kN (C), BF: 3.75 kN (T), CG: 0, DH: 16.25 kN (T), BG: 8.839 kN (T), DG: 22.98 kN (C)

Answer

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

Answer: FBC = 8.485 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.

ABBCACACB50 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 50·1 − 20·4 → Cy = −6 kN
ΣFy = 0: Ay = 50 − −6 = 56 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 = 4/5.657 = 0.7071, cos γ = 4/5.657 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −−6/0.7071 = 8.485 kN

Answer

FBC = 8.485 kN (tension)
5.Shear force & bending moment

Answer: D (x = 6 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 = 45 kN, R2 = 35 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 = 90, MC = 160, MD = 190 kN·m, ME = 140, MF = 70, MG = 0

Answer

Mark D: MD = 190 kN·m
6.Shear force & bending moment

Answer: E (x = 4 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 = 15 kN, R2 = 85 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 = 12.5, MC = 20, MD = −22.5, ME = −70 kN·m, MF = −35, MG = 0

Answer

Mark E: ME = −70 kN·m
7.Beam deflection

Answer: δB = 6.944 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 = 5000 N, a = 1000 mm, L = 4000 mm
EI = 1.32 × 10¹² N·mm²

Deflection at the free end

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

δP = Pa³/(3EI) = 1.263 mm
θP = Pa²/(2EI) = 0.001894 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 6.944 mm

Answer

δB = 6.944 mm
8.Beam deflection

Answer: δmax = 5.625 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 = 15000 N, w = 4 N/mm, L = 6000 mm, EI = 2.4 × 10¹³ N·mm²

Each load on its own

δP = PL³/(48EI) = 15000·6000³/(48·2.4 × 10¹³) = 2.813 mm
δw = 5wL⁴/(384EI) = 5·4·6000⁴/(384·2.4 × 10¹³) = 2.813 mm

Add them

δmax = 2.813 + 2.813 = 5.625 mm

Answer

δmax = 5.625 mm
9.Column buckling

Answer: Pcr = 8.188 kN

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

Smallest second moment of area

A rectangle buckles about its weak axis, using the smaller dimension cubed.

Imin = h·b³/12 = 80·40³/12 = 426667 mm⁴

Effective length

KL = 2·3000 = 6000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·426667/6000² = 8188 N = 8.188 kN

Answer

Pcr = 8.188 kN
10.Column buckling

Answer: d = 28.89 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 = 2·15000 = 30000 N
KL = 0.5·3000 = 1500 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·30000·1500²/(π³·200000))^(1/4) = 28.89 mm

Answer

d = 28.89 mm

Check: the slenderness KL/r is 207.7, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 2.466 × 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 rectangles

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

base: A1 = 300·8 = 2400 mm², y1 = 4 mm
two legs: A2 = 2·8·82 = 1312 mm², y2 = 8 + 82/2 = 49 mm

Centroid

ȳ = (2400·4 + 1312·49)/3712 = 19.91 mm

Parallel-axis theorem

base: 300·8³/12 + 2400·(4 − 19.91)² = 619939 mm⁴
two legs: 2·8·82³/12 + 1312·(49 − 19.91)² = 1.846 × 10⁶ mm⁴
Ix = 619939 + 1.846 × 10⁶
Ix = 2.466 × 10⁶ mm⁴ = 2.466 × 10⁶ mm⁴

Answer

Ix = 2.466 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 59.37 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 = 300·20 = 6000 mm², yf = 160 + 20/2 = 170 mm
web: Aw = 12·160 = 1920 mm², yw = 160/2 = 80 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (6000·170 + 1920·80)/7920 = 148.2 mm

Parallel-axis theorem

flange: 300·20³/12 + 6000·(170 − 148.2)² = 3.056 × 10⁶ mm⁴
web: 12·160³/12 + 1920·(80 − 148.2)² = 1.302 × 10⁷ mm⁴
Ix = 3.056 × 10⁶ + 1.302 × 10⁷ = 1.608 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 180 − 148.2 = 31.82 mm
σ = M·y/I = 3 × 10⁷·31.82/1.608 × 10⁷ = 59.37 MPa

Answer

σtop = 59.37 MPa
13.Effective stress in soil

Answer: σ′ = 92.07 kPa

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

Total stress

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

σ = γd·zw + γsat·(z − zw) = 15·4 + 20.5·3 = 121.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·3 = 29.43 kPa

Effective stress

σ′ = σ − u = 121.5 − 29.43 = 92.07 kPa

Answer

σ′ = 92.07 kPa
14.Effective stress in soil

Answer: σ′ = 91.61 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·1 + γsat,sand·5 + γsat,clay·3.5
σ = 15.5·1 + 20·5 + 17·3.5 = 175 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·8.5 = 83.39 kPa

Effective stress

σ′ = σ − u = 175 − 83.39 = 91.61 kPa

Answer

σ′ = 91.61 kPa
15.Consolidation settlement

Answer: S = 21.05 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 + 45 = 140 kPa ≤ 195 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·4/(1 + 0.6)·log₁₀(140/95) = 21.05 mm

Answer

S = 21.05 mm
16.Consolidation settlement

Answer: t = 1.814 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 = 3 m

Time

t = Tv·Hdr²/cv = 0.403·3²/2 = 1.814 years

Answer

t = 1.814 years
17.Hydrostatic force

Answer: F = 294.3 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 + 2/2 = 5 m
A = H·b = 2·3 = 6 m²
gated = 4 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·5·6 = 294.3 kN

Answer

F = 294.3 kN
18.Hydrostatic force

Answer: F = 43.26 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 = 3 + 1/2 = 3.5 m
A = H·b = 1·1 = 1 m²
gated = 3 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·3.5·1 = 43.26 kN

Answer

F = 43.26 kN
19.Pipe friction & head loss

Answer: hf = 3.636 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 = 0.01/0.007854 = 1.273 m/s

Velocity head

V²/(2g) = 1.273²/(2·9.81) = 0.08263 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.022·(200/0.1)·1.273²/(2·9.81) = 3.636 m

Answer

hf = 3.636 m
20.Pipe friction & head loss

Answer: H = 2.454 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 = 0.01/0.007854 = 1.273 m/s
V²/(2g) = 0.08263 m

Loss coefficients

f·L/D = 0.025·100/0.1 = 25
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 + 25 + 3.7)·0.08263 = 2.454 m

Answer

H = 2.454 m
21.Open-channel flow (Manning)

Answer: Q = 0.2156 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 = 0.2209 m², R = D/4 = 0.1875 m

Velocity

V = (1/0.013)·0.18752/3·0.00151/2 = 0.976 m/s

Flow rate

Q = A·V = 0.2209·0.976 = 0.2156 m³/s

Answer

Q = 0.2156 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003038 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 = (3.5 + 1.5·0.9)·0.9 = 4.365 m²
P = b + 2y·√(1 + z²) = 3.5 + 2·0.9·√(1 + 1.5²) = 6.745 m
R = A/P = 0.6471 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.03·6/(4.365·0.7482) = 0.05512
S = 0.05512² = 0.003038

Answer

S = 0.003038

That is a fall of 3.038 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 12.46 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 = 1000·9.81·0.02·54 = 10.59 kW

Shaft power

Pshaft = Ph/η = 10.59/0.85 = 12.46 kW

Answer

Pshaft = 12.46 kW
24.Pumps & pump power

Answer: H = 23.99 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 = 0.08/0.03142 = 2.546 m/s
V²/(2g) = 0.3305 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (9 + 2.5)·0.3305 = 3.801 m

Pressure head

p/(ρ·g) = 100000/(1000·9.81) = 10.19 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 10 + 10.19 + 3.801 = 23.99 m

Answer

H = 23.99 m
25.Time value of money

Answer: PV = 57350 €

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.

Annuity factor

(1 − (1 + i)−n)/i = (1 − 0.3118)/0.06 = 11.47

Present value

PV = 5 000·11.47 = €57 349.61

Answer

PV = €57 349.61
26.Time value of money

Answer: B = 65309 €

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

Monthly payment

i = 0.002, N = 360
A = 250 000·0.002/(1 − (1 + 0.002)−360) = €974.85

Present value of the remaining payments

Whatever is still owed must be exactly paid off by the remaining payments.

N − k = 360 − 288 = 72
B = 974.9·(1 − (1 + 0.002)−72)/0.002 = €65 309.19

Answer

B = €65 309.19
27.NPV & IRR

Answer: NPV = 5058 €

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 = −45 000
CF1/(1 + 0.09)1 = 12 000/1.09 = 11 009.17
CF2/(1 + 0.09)2 = 21 000/1.188 = 17 675.28
CF3/(1 + 0.09)3 = 13 000/1.295 = 10 038.39
CF4/(1 + 0.09)4 = 16 000/1.412 = 11 334.80

Add them up

NPV = €5 057.64

Answer

NPV = €5 057.64

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

28.NPV & IRR

Answer: MIRR = 22.59 %

Modified IRR: compound every inflow forward to the end of the project at the reinvestment rate (usually the cost of capital) to get the terminal value TV. MIRR is the rate that turns the initial investment into TV: MIRR = (TV/C₀)^(1/n) − 1.

Terminal value of the inflows

28 500·1.083 = 35 901.79
28 000·1.082 = 32 659.20
17 000·1.081 = 18 360.00
26 000·1.080 = 26 000.00
TV = 112 920.99

MIRR

MIRR = (112 920.99/50 000)1/4 − 1 = 22.59%

Answer

MIRR = 22.59%
29.Normal distribution

Answer: P = 0.6915

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 = 320 g, σT = 1.2·√8 = 3.394 g

Standardise

z = (318.3 − 320)/3.394 = −0.5

Probability

P = 1 − Φ(−0.5) = 0.6915

Answer

P = 0.6915
30.Normal distribution

Answer: x = 261.6 g

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) = 0.99 → z = 2.326

Back to x

x = 250 + 2.326·5 = 261.63 g

Answer

x = 261.63 g

This is independent practice material. ExamProblems is not affiliated with or endorsed by the organisation that runs this exam, and the exam name is used only to describe the content. The FE exam is run by NCEES, which is not affiliated with ExamProblems and does not endorse it.

ExamProblems · examproblems.com/courses/fe-exam-civil