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
P1​ = 50 kNP2​ = 60 kNABRA​RB​ = ?2 m2 m4 m

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

L = 8 mP1 = 50 kN at 2 mP2 = 60 kN at 4 m
RB = kN
2.Beam support reactionsHard
P = 40 kNQ = 60 kNADCRD​ = ?2 m3 m3 m2 m

A compound beam is fixed to the wall at A, has an internal hinge at C (5 m from A) and rests on a roller at D (10 m from A). It carries a point load P at 8 m from A and a point load Q at 2 m from A. Find the reaction RD at the roller.

AC = 5 mAD = 10 mP = 40 kN at 8 mQ = 60 kN at 2 m
RD = kN
3.Truss: method of jointsMedium
ABBCACACB50 kN5 m4 m4 m

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

span = 5 mheight = 4 mB is 4 m from Avertical load = 50 kN
FAC = kN
4.Truss: method of jointsHard
ABBCACACB40 kN30 kN8 m6 m2 m

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

span = 8 mheight = 2 mB is 6 m from Avertical load = 40 kNhorizontal load = 30 kN →
FBC = kN
5.Shear force & bending momentMedium
w = 2 kN/mABsection2.5 m5.5 m

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

L = 8 mw = 2 kN/m from 0 to 8 mx = 2.5 m
Vx = kN
6.Shear force & bending momentHard
30 kN50 kN15 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.

30 kN @ 0 m50 kN @ 12 m15 kN @ 6 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)
7.Beam deflectionMedium
w = 8 kN/mδL = 3 m

A cantilever carries a uniformly distributed load w over its whole length. Find the deflection δ at the free end.

w = 8 kN/mL = 3 mE = 70 GPa (aluminium)I = 84 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 8 kN/mP = 2 kNδL = 8 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 = 2 kNw = 8 kN/mL = 8 mE = 70 GPa (aluminium)I = 120 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 1 m20 × 100 mmcross-section

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

L = 1 mE = 70 GPa (aluminium)b × h = 20 × 100 mm
Pcr = kN
10.Column bucklingHard
P = 60 kNL = 1.5 md = ?cross-section

A solid round column of length L made of aluminium is pinned at both ends. It must carry 60 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 60 kNn = 3L = 1.5 mE = 70 GPa (aluminium)
d = mm
11.Centroid & second moment of areaMedium
200 mm150 mm45 mmØ60xIx​ = ?

A 200 mm × 150 mm plate has a circular hole of diameter 60 mm on its vertical centre line, with its centre 45 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 200 mmh = 150 mmd = 60 mmhole centre: y = 45 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1405002210xM = 80 kN·mdimensions in mm

A symmetric I-section has flanges 140 mm wide and 22 mm thick, an overall depth of 500 mm and a web 10 mm thick. It carries a bending moment of 80 kN·m about the axis x. Find the size of the bending stress σj at the junction of the web and the top flange.

B = 140 mmH = 500 mmtf = 22 mmtw = 10 mmM = 80 kN·m
σj = MPa
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 20 kN/m³9 mwater tableXz = 3 m

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

z = 3 mzw = 2 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 19 kN/m³4 mclayγsat​ = 17 kN/m³6 mwater tableXz = 7 m

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

z = 7 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 19 kN/m³clay: γsat = 17 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 100 kPasandclayCc​ = 0.5, Cr​ = 0.04e0​ = 0.95σ′0​ = 120 kPaσ′p​ = 170 kPa4.5 mwater table

A 4.5 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.04 and e₀ = 0.95. At its mid-depth the effective vertical stress is 120 kPa and the preconsolidation pressure is 170 kPa. A new building adds 100 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 4.5 mCc = 0.5Cr = 0.04e0 = 0.95σ′0 = 120 kPaσ′p = 170 kPaΔσ = 100 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 7 mcv​ = 3 m²/year7 mimpervious rockwater table

A clay layer 7 m thick has a coefficient of consolidation cv = 3 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 60% average consolidation the time factor is Tv = 0.287. How many years t does the layer take to reach 60% consolidation?

H = 7 mcv = 3 m²/yearU = 60%Tv = 0.287single drainage
t = years
17.Hydrostatic forceMedium
gated = 1.5 mH = 2 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, 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 = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 0.5 mH = 3 m

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

d = 0.5 mH = 3 mb = 2 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 60 L/sD = 200 mmL = 1000 mf = 0.02

Water flows at 60 L/s through a pipe 1000 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.02 and g = 9.81 m/s². Find the friction head loss hf.

Q = 60 L/sL = 1000 mD = 200 mmf = 0.02g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5free outletH = ?L = 100 m, D = 200 mm, f = 0.0153× bend (K = 0.3)

A pipe 100 m long with an inside diameter of 200 mm (Darcy friction factor f = 0.015) 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), 3 bends (K = 0.3 each) and a valve (K = 5). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 50 L/s?

Q = 50 L/sL = 100 mD = 200 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5
H = m
21.Open-channel flow (Manning)Medium
D = 750 mmn = 0.013, S = 0.003

A concrete storm sewer with an inside diameter of 750 mm flows half full. Manning n = 0.013 and the slope is S = 0.003. Find the flow rate Q in m³/s.

D = 750 mmn = 0.013S = 0.003
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 600 mmn = 0.013, V = 1.2 m/s

A concrete sewer with an inside diameter of 600 mm (Manning n = 0.013) must reach a self-cleansing velocity of 1.2 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 600 mmn = 0.013V = 1.2 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 150 L/sH = 64 m

A pump with an efficiency of 70% delivers 150 L/s of water (ρ = 1000 kg/m³) against a head of 64 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 150 L/sH = 64 mη = 70%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
200 kPa (gauge)PQ = 120 L/sΔz = 26 mL = 150 m, D = 250 mm, f = 0.015, ΣK = 5

A pump moves 120 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 26 m higher. The pipe is 150 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 5 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 200 kPa. Find the head H the pump must add.

Q = 120 L/sΔz = 26 mL = 150 mD = 250 mmf = 0.015ΣK = 5ptank = 200 kPa
H = m
25.Time value of moneyMedium
years01234PV = ?€15 000

You need €15 000 in 4 years. An account pays 3.6% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €15 0003.6% / 4n = 4
PV = €
26.Time value of moneyHard
months0123…N = ?€15 000€450€450€450€4504.8% / 12

You borrow €15 000 at 4.8% per year, compounded monthly, and repay €450 at the end of every month. How many months does it take until the loan is repaid (the last payment may be smaller)? Give the number of payments N.

P = €15 000A = €4504.8% / 12
N = payments
27.NPV & IRRMedium
years01234−30 00012 0009 0007 0008 000

An investment of €30 000 gives these cash flows at the end of years 1 to 4: €12 000, €9 000, €7 000, €8 000. The cost of capital is 6%. Find the net present value NPV.

r = 6%CF0 = −30 000CF1 = 12 000CF2 = 9 000CF3 = 7 000CF4 = 8 000
NPV = €
28.NPV & IRRHard
years0123−20 0009 0007 50012 500

A project costs €20 000 and returns €9 000, €7 500, €12 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −20 000CF1 = 9 000CF2 = 7 500CF3 = 12 500
IRR = %
29.Normal distributionMedium
3237.1P = ?

The delivery times are normally distributed with mean 32 min and standard deviation 6 min. What fraction lies between 32 and 37.1 min? Give P as a decimal.

μ = 32σ = 6x1 = 32x2 = 37.1
P =
30.Normal distributionHard
10 cm0X − Y?

The heights X of men and Y of women in a group are independent and normal: X has mean 180 cm and standard deviation 10 cm, Y has mean 170 cm and standard deviation 12 cm. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 180 cm, σX = 10 cmμY = 170 cm, σY = 12 cm
P =

3Solutions

1.Beam support reactions

Answer: RB = 42.5 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.

P1​ = 50 kNP2​ = 60 kNABRA​RB​2 m2 m4 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·8 = 50·2 + 60·4
RB = 340/8 = 42.5 kN
ΣFy = 0: RA = 110 − 42.5 = 67.5 kN

Answer

RB = 42.5 kN
2.Beam support reactions

Answer: RD = 24 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. 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.

ΣMC = 0: RD·5 = 40·3
RD = 24 kN
VC = 40 − 24 = 16 kN

Answer

RD = 24 kN
3.Truss: method of joints

Answer: FAC = 10 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 50·4 → Cy = 40 kN
ΣFy = 0: Ay = 50 − 40 = 10 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 = 4/4.123 = 0.9701, cos γ = 1/4.123 = 0.2425
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −40/0.9701 = −41.23 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−41.23)·0.2425 = 10 kN

Answer

FAC = 10 kN (tension)
4.Truss: method of joints

Answer: FBC = −53.03 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.

ABBCACACB40 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 40·6 + 30·2 → Cy = 37.5 kN
ΣFy = 0: Ay = 40 − 37.5 = 2.5 kN
ΣFx = 0: Ax = −30 kN

Joint C

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

sin γ = 2/2.828 = 0.7071, cos γ = 2/2.828 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −37.5/0.7071 = −53.03 kN

Answer

FBC = −53.03 kN (compression)
5.Shear force & bending moment

Answer: Vx = 3 kN

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 = 2·8 = 16 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 2·8·4
RB = 64/8 = 8 kN
ΣFy = 0: RA = 16 − 8 = 8 kN
w = 2 kN/mABRA​ = 8RB​ = 8section2.5 m5.5 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.

V = RA − (all downward loads left of the cut)
Vx = 8 − 2·2.5 = 3 kN

Answer

Vx = 3 kN
6.Shear force & bending moment

Answer: E (x = 8 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 = 11.67 kN, R2 = 83.33 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 = −60, MC = −96.67, MD = −133.3, ME = −200 kN·m, MF = −100, MG = 0

Answer

Mark E: ME = −200 kN·m
7.Beam deflection

Answer: δ = 13.78 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 = 8 N/mm, L = 3000 mm
EI = 5.88 × 10¹² N·mm²

Deflection

δ = wL⁴/(8EI) = 8·3000⁴/(8·5.88 × 10¹²) = 13.78 mm

Answer

δ = 13.78 mm
8.Beam deflection

Answer: δmax = 53.33 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 = 2000 N, w = 8 N/mm, L = 8000 mm, EI = 8.4 × 10¹² N·mm²

Each load on its own

δP = PL³/(48EI) = 2000·8000³/(48·8.4 × 10¹²) = 2.54 mm
δw = 5wL⁴/(384EI) = 5·8·8000⁴/(384·8.4 × 10¹²) = 50.79 mm

Add them

δmax = 2.54 + 50.79 = 53.33 mm

Answer

δmax = 53.33 mm
9.Column buckling

Answer: Pcr = 94 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 = 100·20³/12 = 66667 mm⁴

Effective length

KL = 0.7·1000 = 700 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·66667/700² = 93996 N = 94 kN

Answer

Pcr = 94 kN
10.Column buckling

Answer: d = 58.79 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 = 3·60000 = 180000 N
KL = 1·1500 = 1500 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·180000·1500²/(π³·70000))^(1/4) = 58.79 mm

Answer

d = 58.79 mm

Check: the slenderness KL/r is 102.1, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 52.8 × 10⁶ mm⁴

Sections with holes: treat a hole as a negative area. The centroid is ȳ = (A₁y₁ − A₂y₂)/(A₁ − A₂), with A₁, y₁ for the full plate and A₂, y₂ for the hole. For the second moment of area about the centroidal axis, use the parallel-axis theorem for each part and subtract the hole: I = (Ic1 + A₁d₁²) − (Ic2 + A₂d₂²), where d is the distance from each part's own centroid to the axis through ȳ. A rectangle has Ic = bh³/12 and a circle Ic = πd⁴/64.

Centroid

ȳ = (30000·75 − 2827·45)/(30000 − 2827) = 78.12 mm

Full plate about ȳ

200·150³/12 + 30000·−3.122² = 56.54 × 10⁶ mm⁴

Hole about ȳ

π·60⁴/64 + 2827·−33.12² = 3.738 × 10⁶ mm⁴

Subtract

Ix = 52.8 × 10⁶ mm⁴

Answer

Ix = 52.8 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σj = 42.31 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.

Outer rectangle minus the two side cut-outs

Both cut-outs together are (B − tw) wide and hw = H − 2tf high, and share the axis x.

hw = 500 − 2·22 = 456 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (140·500³ − 130·456³)/12
Ix = 4.311 × 10⁸ mm⁴

Bending stress

y = 250 − 22 = 228 mm
σ = M·y/I = 8 × 10⁷·228/4.311 × 10⁸ = 42.31 MPa

Answer

σj = 42.31 MPa
13.Effective stress in soil

Answer: σ′ = 40.19 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) = 15·2 + 20·1 = 50 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·1 = 9.81 kPa

Effective stress

σ′ = σ − u = 50 − 9.81 = 40.19 kPa

Answer

σ′ = 40.19 kPa
14.Effective stress in soil

Answer: σ = 115 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 = 15·3 + 19·1 + 17·3 = 115 kPa

Answer

σ = 115 kPa
15.Consolidation settlement

Answer: S = 143.2 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 = 120 + 100 = 220 kPa > 170 kPa

Settlement

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

S = 0.04·4.5/(1 + 0.95)·log₁₀(170/120) + 0.5·4.5/(1 + 0.95)·log₁₀(220/170)
S = 13.96 + 129.2 = 143.2 mm

Answer

S = 143.2 mm
16.Consolidation settlement

Answer: t = 4.688 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 = 7 m

Time

t = Tv·Hdr²/cv = 0.287·7²/3 = 4.688 years

Answer

t = 4.688 years
17.Hydrostatic force

Answer: F = 147.2 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 = 2·3 = 6 m²
gated = 1.5 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.5·6 = 147.2 kN

Answer

F = 147.2 kN
18.Hydrostatic force

Answer: F = 120.7 kN

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

Centroid depth and area

yc = d + H/2 = 0.5 + 3/2 = 2 m
A = H·b = 3·2 = 6 m²
gated = 0.5 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·2·6 = 120.7 kN

Answer

F = 120.7 kN
19.Pipe friction & head loss

Answer: hf = 18.59 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·0.2²/4 = 0.03142 m²
V = Q/A = 0.06/0.03142 = 1.91 m/s

Velocity head

V²/(2g) = 1.91²/(2·9.81) = 0.1859 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.02·(1000/0.2)·1.91²/(2·9.81) = 18.59 m

Answer

hf = 18.59 m
20.Pipe friction & head loss

Answer: H = 1.924 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 = 0.05/0.03142 = 1.592 m/s
V²/(2g) = 0.1291 m

Loss coefficients

f·L/D = 0.015·100/0.2 = 7.5
ΣK = 0.5 + 3·0.3 + 5 = 6.4

Energy equation

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

H = (1 + 7.5 + 6.4)·0.1291 = 1.924 m

Answer

H = 1.924 m
21.Open-channel flow (Manning)

Answer: Q = 0.3049 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)·0.18752/3·0.0031/2 = 1.38 m/s

Flow rate

Q = A·V = 0.2209·1.38 = 0.3049 m³/s

Answer

Q = 0.3049 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003053 m/m

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

Hydraulic radius

R = D/4 = 0.6/4 = 0.15 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·1.2/0.2823)² = 0.003053

Answer

S = 0.003053

That is a fall of 3.053 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 134.5 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 = 1000·9.81·0.15·64 = 94.18 kW

Shaft power

Pshaft = Ph/η = 94.18/0.7 = 134.5 kW

Answer

Pshaft = 134.5 kW
24.Pumps & pump power

Answer: H = 50.65 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (9 + 5)·0.3046 = 4.264 m

Pressure head

p/(ρ·g) = 200000/(1000·9.81) = 20.39 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 26 + 20.39 + 4.264 = 50.65 m

Answer

H = 50.65 m
25.Time value of money

Answer: PV = 12997 €

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 = 0.036000000000000004/4 = 0.009
N = 4·4 = 16

Present value

PV = FV/(1 + i)N = 15 000/1.154 = €12 996.69

Answer

PV = €12 996.69
26.Time value of money

Answer: N = 36 payments

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.

Rearrange the annuity formula

i = 0.004
(1 + i)−N = 1 − 15 000·0.004/450 = 0.8667

Solve with logarithms

N = −ln(0.8667)/ln(1.004) = 35.85

Round up to whole payments

35 full payments leave a small balance, which the last, smaller payment clears.

N = 36

Answer

N = 36 payments
27.NPV & IRR

Answer: NPV = 1545 €

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

Present value of each cash flow

CF0 = −30 000
CF1/(1 + 0.06)1 = 12 000/1.06 = 11 320.75
CF2/(1 + 0.06)2 = 9 000/1.124 = 8 009.97
CF3/(1 + 0.06)3 = 7 000/1.191 = 5 877.33
CF4/(1 + 0.06)4 = 8 000/1.262 = 6 336.75

Add them up

NPV = €1 544.81

Answer

NPV = €1 544.81

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

28.NPV & IRR

Answer: IRR = 19.83 %

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(15%) = 1 716.12
NPV(20%) = −57.87

Narrow down

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

IRR ≈ 15 + 5·1 716.12/(1 716.12 − (−57.87)) = 19.84%
exact: NPV(19.83%) = 0 → IRR = 19.83%

Answer

IRR = 19.83%
29.Normal distribution

Answer: P = 0.3023

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 = (32 − 32)/6 = 0
z₂ = (37.1 − 32)/6 = 0.85

Area between

P = Φ(0.85) − Φ(0) = 0.8023 − 0.5 = 0.3023

Answer

P = 0.3023
30.Normal distribution

Answer: P = 0.7389

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 = 180 − 170 = 10 cm, σ = 15.62 cm

Standardise

z = (0 − 10)/15.62 = −0.64

Probability

P = 1 − Φ(−0.64) = 0.7389

Answer

P = 0.7389

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