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​ = 25 kNP2​ = 50 kNABRA​ = ?RB​6 m1 m3 m

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

L = 10 mP1 = 25 kN at 6 mP2 = 50 kN at 7 m
RA = kN
2.Beam support reactionsHard
P = 60 kN, 50°Q = 10 kNABRA​ = ?0.5 m3 m1.5 m

The simply supported beam has a pin at A and a roller at B. A load P acts at 3.5 m from A, inclined at 50° to the horizontal, and a vertical load Q acts at 0.5 m from A. Find the magnitude of the total reaction force RA at the pin A.

L = 5 mP = 60 kN at 3.5 m, θ = 50°Q = 10 kN at 0.5 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB50 kN4 m1 m3 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 = 3 mB is 1 m from Avertical load = 50 kN
FBC = kN
4.Truss: method of jointsHard
ABBCACACB50 kN10 kN4 m3 m3 m

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

span = 4 mheight = 3 mB is 3 m from Avertical load = 50 kNhorizontal load = 10 kN ←
FAC = kN
5.Shear force & bending momentMedium
10 kN/m35 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.

35 kN @ 6 m10 kN/m, 4–12 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
w = 12 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 bending moment MB at support B. Use sagging moments positive and upward shear on the left face positive.

L = 5.5 mw = 12 kN/m from 0 to 5.5 msupports at x = 0 and x = 4 m
MB = kN·m
7.Beam deflectionMedium
P = 17 kNABδ1.5 m3.5 m

A cantilever of length L is fixed at A and carries a point load P at a distance a = 1.5 m from A. Find the deflection δB at the free end B.

P = 17 kNa = 1.5 mL = 5 mE = 200 GPa (steel)I = 57 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
P = 15 kNAB3 m3 m

A propped cantilever is fixed at A and simply supported (propped) at B. It carries a point load P at midspan. EI is constant. Find the reaction RB at the prop.

L = 6 mP = 15 kN at 3 m
RB = kN
9.Column bucklingMedium
PL = 2 m50 × 60 mmcross-section

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

L = 2 mE = 200 GPa (steel)b × h = 50 × 60 mm
Pcr = kN
10.Column bucklingHard
PL = 2.5 md = 30 mmcross-section

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

L = 2.5 mE = 70 GPa (aluminium)d = 30 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1401512016xdimensions in mm

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

bf = 140 mmtf = 15 mmtw = 16 mmhw = 120 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
190300143501410xdimensions in mm

A welded I-section has a top flange 190 × 14 mm, a web 350 mm high and 10 mm thick, and a bottom flange 300 × 14 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 190 × 14 mmweb: 10 × 350 mmbottom flange: 300 × 14 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 17 kN/m³γsat​ = 20 kN/m³7 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 = 17 kN/m³sand: γsat = 20 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 18.5 kN/m³4 mclayγsat​ = 18 kN/m³4 mwater tableXz = 6 m

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

z = 6 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 18.5 kN/m³clay: γsat = 18 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 110 kPasandclayCc​ = 0.3, Cr​ = 0.03e0​ = 0.7σ′0​ = 115 kPaσ′p​ = 145 kPa5.5 mwater table

A 5.5 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.03 and e₀ = 0.7. At its mid-depth the effective vertical stress is 115 kPa and the preconsolidation pressure is 145 kPa. A new building adds 110 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 5.5 mCc = 0.3Cr = 0.03e0 = 0.7σ′0 = 115 kPaσ′p = 145 kPaΔσ = 110 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 7.5 m7.5 mimpervious rockwater table

In a laboratory oedometer test, a clay specimen 25 mm thick, drained at the top and bottom, reaches 50% consolidation in 5 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 = 25 mmtlab = 5 minH = 7.5 mfield: single drainage
t = days
17.Hydrostatic forceMedium
gated = 2 mH = 3 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 3 mb = 1.5 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 = 120 L/sD = 300 mmL = 100 mf = 0.015

Water flows at 120 L/s through a pipe 100 m long with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the friction head loss hf.

Q = 120 L/sL = 100 mD = 300 mmf = 0.015g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10free outletH = ?L = 500 m, D = 300 mm, f = 0.0154× bend (K = 0.3)

A pipe 500 m long with an inside diameter of 300 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), 4 bends (K = 0.3 each) and a valve (K = 10). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 80 L/s?

Q = 80 L/sL = 500 mD = 300 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10
H = m
21.Open-channel flow (Manning)Medium
b = 2.5 my = 1 mn = 0.025, S = 0.0008

A rectangular gravel channel is 2.5 m wide. Water flows uniformly 1 m deep. Manning n = 0.025 and the bed slope is S = 0.0008. Find the flow rate Q in m³/s.

b = 2.5 my = 1 mn = 0.025S = 0.0008
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 200 mmn = 0.013, V = 0.6 m/s

A concrete sewer with an inside diameter of 200 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.6 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 200 mmn = 0.013V = 0.6 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 10 L/sH = 72 m

A pump delivers 10 L/s of water (ρ = 1000 kg/m³) against a head of 72 m. The pump efficiency is 70% and the electric motor driving it has an efficiency of 94%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 10 L/sH = 72 mηpump = 70%ηmotor = 94%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 80 L/sΔz = 5 mL = 200 m, D = 200 mm, f = 0.015, ΣK = 3

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 5 m higher. The pipe is 200 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 3 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 80 L/sΔz = 5 mL = 200 mD = 200 mmf = 0.015ΣK = 3
H = m
25.Time value of moneyMedium
years0123456PV = ?€15 000

You need €15 000 in 6 years. An account pays 6% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €15 0006% / 4n = 6
PV = €
26.Time value of moneyHard
months0123…300€150 000AAAA7.2% / 12, I = ?

A loan of €150 000 is repaid with equal monthly payments over 25 years at 7.2% per year, compounded monthly. How much interest I is paid in total over the life of the loan?

P = €150 0007.2% / 12N = 300
I = €
27.NPV & IRRMedium
years0123−45 00017 00019 00010 000

An investment of €45 000 gives these cash flows at the end of years 1 to 3: €17 000, €19 000, €10 000. The cost of capital is 12%. Find the net present value NPV.

r = 12%CF0 = −45 000CF1 = 17 000CF2 = 19 000CF3 = 10 000
NPV = €
28.NPV & IRRHard
years0123−20 00012 0008 0008 000

A project costs €20 000 and returns €12 000, €8 000, €8 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −20 000CF1 = 12 000CF2 = 8 000CF3 = 8 000
IRR = %
29.Normal distributionMedium
82115P = ?

The IQ scores are normally distributed with mean 100 points and standard deviation 15 points. What fraction lies between 82 and 115 points? Give P as a decimal.

μ = 100σ = 15x1 = 82x2 = 115
P =
30.Normal distributionHard
4 s0X − Y?

Runner A's lap time X and runner B's lap time Y are independent and normal: X has mean 52 s and standard deviation 4 s, Y has mean 48 s and standard deviation 3 s. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 52 s, σX = 4 sμY = 48 s, σY = 3 s
P =

3Solutions

1.Beam support reactions

Answer: RA = 25 kN

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

P1​ = 25 kNP2​ = 50 kNABRA​RB​6 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.

ΣMA = 0: RB·10 = 25·6 + 50·7
RB = 500/10 = 50 kN
ΣFy = 0: RA = 75 − 50 = 25 kN

Answer

RA = 25 kN
2.Beam support reactions

Answer: RA = 44.8 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.

Components of P

Pv = 60·sin 50° = 45.96 kN
Ph = 60·cos 50° = 38.57 kN

Reactions

ΣMA = 0: RB·5 = 45.96·3.5 + 10·0.5 → RB = 33.17 kN
Ay = 45.96 + 10 − 33.17 = 22.79 kN
Ax = Ph = 38.57 kN

Resultant at A

RA = √(38.57² + 22.79²) = 44.8 kN

Answer

RA = 44.8 kN
3.Truss: method of joints

Answer: FBC = −17.68 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·4 = 50·1 → Cy = 12.5 kN
ΣFy = 0: Ay = 50 − 12.5 = 37.5 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 = 3/4.243 = 0.7071, cos γ = 3/4.243 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −12.5/0.7071 = −17.68 kN

Answer

FBC = −17.68 kN (compression)
4.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 kN10 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·4 = 50·3 − 10·3 → Cy = 30 kN
ΣFy = 0: Ay = 50 − 30 = 20 kN
ΣFx = 0: Ax = 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 = 3/3.162 = 0.9487, cos γ = 1/3.162 = 0.3162
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −30/0.9487 = −31.62 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−31.62)·0.3162 = 10 kN

Answer

FAC = 10 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 = 44.17 kN, R2 = 70.83 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 = 88.33, MC = 176.7, MD = 245 kN·m, ME = 203.3, MF = 121.7, MG = 0

Answer

Mark D: MD = 245 kN·m
6.Shear force & bending moment

Answer: MB = −13.5 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut. 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 = 12·5.5 = 66 kN, acting at x̄ = 2.75 m
ΣMA = 0: RB·4 = 12·5.5·2.75
RB = 181.5/4 = 45.38 kN
ΣFy = 0: RA = 66 − 45.38 = 20.63 kN

Cut at B and keep the overhang

The load on the overhang, w·a, acts at a/2 from B and makes the beam hog over the support.

MB = −w·a²/2 = −12·1.5²/2 = −13.5 kN·m

Answer

MB = −13.5 kN·m
7.Beam deflection

Answer: δB = 7.549 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 = 17000 N, a = 1500 mm, L = 5000 mm
EI = 1.14 × 10¹³ N·mm²

Deflection at the free end

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

δP = Pa³/(3EI) = 1.678 mm
θP = Pa²/(2EI) = 0.001678 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 7.549 mm

Answer

δB = 7.549 mm
8.Beam deflection

Answer: RB = 4.688 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 = P(L/2)²(3L − L/2)/(6EI) = 5PL³/(48EI)

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) = 5PL³/(48EI) → RB = 5P/16 = 5·15/16 = 4.688 kN

Answer

RB = 4.688 kN
9.Column buckling

Answer: Pcr = 77.11 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 = 60·50³/12 = 625000 mm⁴

Effective length

KL = 2·2000 = 4000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·625000/4000² = 77106 N = 77.11 kN

Answer

Pcr = 77.11 kN
10.Column buckling

Answer: σcr = 24.87 MPa

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

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·30⁴/64 = 39761 mm⁴

Radius of gyration and slenderness

A = 706.9 mm²
r = √(I/A) = √(39761/706.9) = 7.5 mm
KL = 0.5·2500 = 1250 mm
KL/r = 1250/7.5 = 166.7

Critical stress

σcr = π²E/(KL/r)² = π²·70000/166.7² = 24.87 MPa

Answer

σcr = 24.87 MPa
11.Centroid & second moment of area

Answer: Ix = 6.913 × 10⁶ mm⁴

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

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 140·15 = 2100 mm², yf = 120 + 15/2 = 127.5 mm
web: Aw = 16·120 = 1920 mm², yw = 120/2 = 60 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2100·127.5 + 1920·60)/4020 = 95.26 mm

Parallel-axis theorem

flange: 140·15³/12 + 2100·(127.5 − 95.26)² = 2.222 × 10⁶ mm⁴
web: 16·120³/12 + 1920·(60 − 95.26)² = 4.691 × 10⁶ mm⁴
Ix = 2.222 × 10⁶ + 4.691 × 10⁶ = 6.913 × 10⁶ mm⁴ = 6.913 × 10⁶ mm⁴

Answer

Ix = 6.913 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 255.5 × 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 = 2660 mm², y = 371 mm
web: A = 3500 mm², y = 189 mm
bottom flange: A = 4200 mm², y = 7 mm

Centroid

ȳ = (2660·371 + 3500·189 + 4200·7)/10360 = 161.9 mm

Parallel-axis theorem

top flange: 190·14³/12 + 2660·209.1² = 1.163 × 10⁸ mm⁴
web: 10·350³/12 + 3500·27.05² = 3.829 × 10⁷ mm⁴
bottom flange: 300·14³/12 + 4200·154.9² = 1.009 × 10⁸ mm⁴
Ix = 1.163 × 10⁸ + 3.829 × 10⁷ + 1.009 × 10⁸
Ix = 2.555 × 10⁸ mm⁴ = 255.5 × 10⁶ mm⁴

Answer

Ix = 255.5 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ′ = 98.57 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) = 17·4 + 20·3 = 128 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 = 128 − 29.43 = 98.57 kPa

Answer

σ′ = 98.57 kPa
14.Effective stress in soil

Answer: σ′ = 71.57 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·2
σ = 15.5·3 + 18.5·1 + 18·2 = 101 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 = 101 − 29.43 = 71.57 kPa

Answer

σ′ = 71.57 kPa
15.Consolidation settlement

Answer: S = 195 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 = 115 + 110 = 225 kPa > 145 kPa

Settlement

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

S = 0.03·5.5/(1 + 0.7)·log₁₀(145/115) + 0.3·5.5/(1 + 0.7)·log₁₀(225/145)
S = 9.771 + 185.2 = 195 mm

Answer

S = 195 mm
16.Consolidation settlement

Answer: t = 1250 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 = 25/2 = 12.5 mm = 0.0125 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 = 5·(7.5/0.0125)² = 1.8 × 10⁶ min
tfield = 1.8 × 10⁶/1440 = 1250 days

Answer

t = 1250 days
17.Hydrostatic force

Answer: F = 154.5 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 = 2 + 3/2 = 3.5 m
A = H·b = 3·1.5 = 4.5 m²
gated = 2 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.5·4.5 = 154.5 kN

Answer

F = 154.5 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 = 0.7345 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·0.3²/4 = 0.07069 m²
V = Q/A = 0.12/0.07069 = 1.698 m/s

Velocity head

V²/(2g) = 1.698²/(2·9.81) = 0.1469 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.015·(100/0.3)·1.698²/(2·9.81) = 0.7345 m

Answer

hf = 0.7345 m
20.Pipe friction & head loss

Answer: H = 2.461 m

Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.

Velocity

V = Q/A = 0.08/0.07069 = 1.132 m/s
V²/(2g) = 0.06529 m

Loss coefficients

f·L/D = 0.015·500/0.3 = 25
ΣK = 0.5 + 4·0.3 + 10 = 11.7

Energy equation

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

H = (1 + 25 + 11.7)·0.06529 = 2.461 m

Answer

H = 2.461 m
21.Open-channel flow (Manning)

Answer: Q = 1.911 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·y = 2.5·1 = 2.5 m²
P = b + 2y = 2.5 + 2·1 = 4.5 m
R = A/P = 0.5556 m

Velocity

V = (1/0.025)·0.55562/3·0.00081/2 = 0.7646 m/s

Flow rate

Q = A·V = 2.5·0.7646 = 1.911 m³/s

Answer

Q = 1.911 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003303 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 = 0.2/4 = 0.05 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.6/0.1357)² = 0.003303

Answer

S = 0.003303

That is a fall of 3.303 m per kilometre.

23.Pumps & pump power

Answer: Pel = 10.73 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 = 1000·9.81·0.01·72 = 7.063 kW

Shaft power

Pshaft = 7.063/0.7 = 10.09 kW

Electrical power

Pel = 10.09/0.94 = 10.73 kW

Answer

Pel = 10.73 kW
24.Pumps & pump power

Answer: H = 10.95 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) = (15 + 3)·0.3305 = 5.949 m

Pump head

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

H = Δz + hL = 5 + 5.949 = 10.95 m

Answer

H = 10.95 m
25.Time value of money

Answer: PV = 10493 €

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 = 0.06/4 = 0.015
N = 4·6 = 24

Present value

PV = FV/(1 + i)N = 15 000/1.43 = €10 493.16

Answer

PV = €10 493.16
26.Time value of money

Answer: I = 173815 €

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 = 0.006, N = 300
A = 150 000·0.006/(1 − (1 + 0.006)−300) = €1 079.38

Total interest

I = N·A − P = 300·1079 − 150 000 = €173 814.91

Answer

I = €173 814.91
27.NPV & IRR

Answer: NPV = −7557 €

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 + 0.12)1 = 17 000/1.12 = 15 178.57
CF2/(1 + 0.12)2 = 19 000/1.254 = 15 146.68
CF3/(1 + 0.12)3 = 10 000/1.405 = 7 117.80

Add them up

NPV = €−7 556.94

Answer

NPV = €−7 556.94

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

28.NPV & IRR

Answer: IRR = 20.64 %

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(20%) = 185.19
NPV(25%) = −1 184.00

Narrow down

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

IRR ≈ 20 + 5·185.19/(185.19 − (−1 184.00)) = 20.68%
exact: NPV(20.64%) = 0 → IRR = 20.64%

Answer

IRR = 20.64%
29.Normal distribution

Answer: P = 0.7263

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 = (82 − 100)/15 = −1.2
z₂ = (115 − 100)/15 = 1

Area between

P = Φ(1) − Φ(−1.2) = 0.8413 − 0.1151 = 0.7263

Answer

P = 0.7263
30.Normal distribution

Answer: P = 0.7881

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 = 52 − 48 = 4 s, σ = 5 s

Standardise

z = (0 − 4)/5 = −0.8

Probability

P = 1 − Φ(−0.8) = 0.7881

Answer

P = 0.7881

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