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
Draw a timeline with every cash flow and its timing.
Match the rate to the period: a monthly rate for monthly payments.
Use FV = PV·(1 + i)ⁿ for single amounts and the annuity formulas for equal payments.
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
List all cash flows with their year; the investment at year 0 is negative.
Discount each cash flow: CFt/(1 + r)t.
Add them up to get the NPV. Positive means the project earns more than r.
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
Convert the value to a z-score: z = (x − μ)/σ.
Look up Φ(z), the area to the left of z.
For the area to the right use 1 − Φ(z); for an interval subtract the two left areas.
For a percentile, work backwards: find z for the area, then x = μ + z·σ.
2Practice problems
1.Beam support reactionsMedium
The beam has a pin at A and a roller at B, 3 m from A, and overhangs B to the free end C. Find the vertical reaction RB, taking upward as positive.
AB = 3 mAC = 4 mP1 = 80 kN at 1 mP2 = 45 kN at 4 m
RB = kN
2.Beam support reactionsHard
The simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RB.
L = 10 mP = 60 kN at 3 mw = 5 kN/m from 0 to 1 m
RB = kN
3.Truss: method of jointsMedium
Use the method of joints to find the force FAB in member AB. Give tension as positive and compression as negative.
span = 6 mheight = 4 mB is 5 m from Avertical load = 10 kN
FAB = kN
4.Truss: method of jointsHard
Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.
D: 35 kN ↓F: 25 kN ↓F: 20 kN →G: 25 kN ↓
1member AB
2member BC
3member CD
4member DE
5member FG
6member GH
7member AF
8member HE
9member BF
10member CG
11member DH
12member FC
13member HC
5.Shear force & bending momentMedium
Find the shear force Vx at the section x = 6 m from support A. Use sagging moments positive and upward shear on the left face positive.
L = 8 mw = 6 kN/m from 0 to 8 mx = 6 m
Vx = kN
6.Shear force & bending momentHard
Find the bending moment Mx at the section x = 4 m from support A. Use sagging moments positive and upward shear on the left face positive.
L = 10 mP = 20 kN at 8 mw = 8 kN/m from 0 to 10 mx = 4 m
Mx = kN·m
7.Beam deflectionMedium
A simply supported beam carries a uniformly distributed load w over its whole span. Find the maximum deflection δmax, at midspan.
w = 6 kN/mL = 2 mE = 11 GPa (timber)I = 36 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
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 size of the bending moment MA at the fixed end.
L = 4 mP = 80 kN at 2 m
MA = kN·m
9.Column bucklingMedium
A column of length L made of steel is fixed at both ends. Using Euler’s formula, find its critical buckling load Pcr.
L = 2 mE = 200 GPa (steel)b × h = 25 × 60 mm
Pcr = kN
10.Column bucklingHard
A solid round column of length L made of steel is fixed at the base and pinned at the top. It must carry 70 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.
P = 70 kNn = 3L = 4 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
A 200 mm × 150 mm plate has a circular hole of diameter 60 mm on its vertical centre line, with its centre 105 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 = 105 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
A 100 mm × 240 mm plate has a rectangular cut-out 30 mm wide and 20 mm high, centred on the vertical centre line with its centre 72 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.
b = 100 mmh = 240 mmcut-out: 30 × 20 mmhole centre: y = 72 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
For the soil profile shown, find the total vertical stress σ at point X.
A 6 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.02 and e₀ = 0.9. At its mid-depth the effective vertical stress is 105 kPa and the preconsolidation pressure is 165 kPa. A new building adds 170 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.
A clay layer 4.5 m thick has a coefficient of consolidation cv = 1 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 90% average consolidation the time factor is Tv = 0.848. How many years t does the layer take to reach 90% consolidation?
A vertical rectangular gate 3 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 = 2 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
A vertical rectangular gate 1.5 m wide sits in the wall of a tank of oil, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.
Water (ρ = 1000 kg/m³) flows at 1.4 m/s through a horizontal pipe, 1000 m long, with an inside diameter of 150 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.
A pipe 200 m long with an inside diameter of 150 mm (Darcy friction factor f = 0.02) 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 = 2). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 20 L/s?
A rectangular unfinished concrete channel is 3 m wide. Water flows uniformly 2.1 m deep. Manning n = 0.014 and the bed slope is S = 0.0015. Find the flow rate Q in m³/s.
b = 3 my = 2.1 mn = 0.014S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
A trapezoidal gravel channel with a bottom width of 5.5 m and side slopes of 1:1 (horizontal:vertical) must carry 16 m³/s in uniform flow at a depth of 1.6 m. Manning n = 0.025. Find the required bed slope S (in m/m).
Q = 16 m³/sb = 5.5 my = 1.6 mz = 1n = 0.025
S = m/m
23.Pumps & pump powerMedium
A pump with an efficiency of 80% delivers 10 L/s of water (ρ = 1000 kg/m³) against a head of 20 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.
Q = 10 L/sH = 20 mη = 80%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
A pump moves 75 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 16 m higher. The pipe is 400 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.
You invest €20 000 at a nominal rate of 3.6% per year, compounded monthly. Find the value FV of the investment after 8 years.
PV = €20 0003.6% / 12n = 8
FV = €
26.Time value of moneyHard
A mortgage of €200 000 is repaid with equal monthly payments over 30 years at 5.4% per year, compounded monthly. How much is still owed just after the payment at the end of year 19? Find the outstanding balance B.
P = €200 0005.4% / 12N = 360k = 228
B = €
27.NPV & IRRMedium
An investment of €45 000 gives these cash flows at the end of years 1 to 4: €15 000, €9 000, €18 000, €13 000. The cost of capital is 10%. Find the net present value NPV.
A project costs €40 000 and returns €27 000, €16 000, €18 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.
CF0 = −40 000CF1 = 27 000CF2 = 16 000CF3 = 18 500
IRR = %
29.Normal distributionMedium
The exam scores are normally distributed with mean 65 points and standard deviation 10 points. What fraction lies between 57 and 85 points? Give P as a decimal.
μ = 65σ = 10x1 = 57x2 = 85
P =
30.Normal distributionHard
The bag weights are normally distributed with mean 250 g and standard deviation 5 g. Find the value x below which 20% of them lie (the 20th percentile).
μ = 250σ = 5P = 20%
x = g
3Solutions
1.Beam support reactions
Answer: RB = 86.67 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·3 = 80·1 + 45·4
RB = 260/3 = 86.67 kN
Vertical equilibrium
RA = 80 + 45 − 86.67 = 38.33 kN
Answer
RB = 86.67 kN
2.Beam support reactions
Answer: RB = 18.25 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.
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 = 5·1 = 5 kN, acting at x̄ = 0.5 m
ΣMA = 0: RB·10 = 60·3 + 5·1·0.5
RB = 182.5/10 = 18.25 kN
ΣFy = 0: RA = 65 − 18.25 = 46.75 kN
Answer
RB = 18.25 kN
3.Truss: method of joints
Answer: FAB = −2.668 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.
Support reactions
Equilibrium of the whole truss. Moments about A, counter-clockwise positive.
ΣMA = 0: Cy·6 = 10·5 → Cy = 8.333 kN
ΣFy = 0: Ay = 10 − 8.333 = 1.667 kN
Joint A
Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.
sin α = 4/6.403 = 0.6247
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −1.667/0.6247 = −2.668 kN
Answer
FAB = −2.668 kN (compression)
4.Truss: method of joints
Answer: member BF
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 B
AB and BC lie on one straight line and the joint carries no load. Balancing forces across that line leaves only BF.
ΣF⊥ = 0 → FBF = 0
Check with the method of joints
Solving all joints gives these member forces (T = tension, C = compression).
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 = 6·8 = 48 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 6·8·4
RB = 192/8 = 24 kN
ΣFy = 0: RA = 48 − 24 = 24 kN
Cut at x = 6 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 = 24 − 6·6 = −12 kN
Answer
Vx = −12 kN
6.Shear force & bending moment
Answer: Mx = 112 kN·m
Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.
Support reactions
Equilibrium of the whole beam.
UDL resultant: W = w·ℓ = 8·10 = 80 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 20·8 + 8·10·5
RB = 560/10 = 56 kN
ΣFy = 0: RA = 100 − 56 = 44 kN
Cut at x = 4 m and keep the left part
Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.
M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 44·4 − 8·4·2 = 112 kN·m
Answer
Mx = 112 kN·m
7.Beam deflection
Answer: δmax = 3.157 mm
Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition).
Consistent units
Work in N and mm: P in N, w in N/mm (kN/m = N/mm), L in mm, E in N/mm² (GPa × 1000), I in mm⁴.
w = 6 N/mm, L = 2000 mm
EI = 3.96 × 10¹¹ N·mm²
Deflection
δmax = 5wL⁴/(384EI) = 5·6·2000⁴/(384·3.96 × 10¹¹) = 3.157 mm
Answer
δmax = 3.157 mm
8.Beam deflection
Answer: MA = 60 kN·m
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.
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.
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 = 3·70000 = 210000 N
KL = 0.7·4000 = 2800 mm
Solve for the diameter
d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·210000·2800²/(π³·200000))^(1/4) = 64.2 mm
Answer
d = 64.2 mm
Check: the slenderness KL/r is 174.4, 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 − 2827·105)/(30000 − 2827) = 71.88 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: Ix = 113.8 × 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 = (24000·120 − 600·72)/(24000 − 600) = 121.2 mm
Full plate about ȳ
100·240³/12 + 24000·−1.231² = 115.2 × 10⁶ mm⁴
Hole about ȳ
30·20³/12 + 600·−49.23² = 1.474 × 10⁶ mm⁴
Subtract
Ix = 113.8 × 10⁶ mm⁴
Answer
Ix = 113.8 × 10⁶ mm⁴
13.Effective stress in soil
Answer: σ = 101 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.
Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).
Pore water pressure
Water pressure grows with depth below the water table.
u = γw·(z − zw) = 9.81·3 = 29.43 kPa
Answer
u = 29.43 kPa
15.Consolidation settlement
Answer: S = 257.6 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 = 105 + 170 = 275 kPa > 165 kPa
Settlement
Recompression up to σ′p, virgin compression beyond it.
S = 0.02·6/(1 + 0.9)·log₁₀(165/105) + 0.35·6/(1 + 0.9)·log₁₀(275/165)
S = 12.4 + 245.2 = 257.6 mm
Answer
S = 257.6 mm
16.Consolidation settlement
Answer: t = 4.293 years
Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.
Drainage path
Hdr = H/2 = 4.5/2 = 2.25 m
Time
t = Tv·Hdr²/cv = 0.848·2.25²/1 = 4.293 years
Answer
t = 4.293 years
17.Hydrostatic force
Answer: F = 176.6 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 + 2/2 = 3 m
A = H·b = 2·3 = 6 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·3·6 = 176.6 kN
Answer
F = 176.6 kN
18.Hydrostatic force
Answer: F = 53.42 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 + 1.5/2 = 2.75 m
A = H·b = 1.5·1.5 = 2.25 m²
Resultant force
F = ρ·g·yc·A = 880·9.81·2.75·2.25 = 53.42 kN
Answer
F = 53.42 kN
19.Pipe friction & head loss
Answer: Δp = 98 kPa
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.
Head loss
hf = f·(L/D)·V²/(2g) = 0.015·(1000/0.15)·1.4²/(2·9.81) = 9.99 m
Pressure drop
The pipe is horizontal and the velocity does not change, so the energy equation reduces to Δp = ρ·g·hf.
Δp = ρ·g·hf = 1000·9.81·9.99 = 98000 Pa = 98 kPa
Answer
Δp = 98 kPa
20.Pipe friction & head loss
Answer: H = 2.028 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 = 0.02/0.01767 = 1.132 m/s
V²/(2g) = 0.06529 m
Loss coefficients
f·L/D = 0.02·200/0.15 = 26.67
ΣK = 0.5 + 3·0.3 + 2 = 3.4
Energy equation
The outlet jet still carries its velocity head; it is not a loss but it has to be supplied.
H = (1 + 26.67 + 3.4)·0.06529 = 2.028 m
Answer
H = 2.028 m
21.Open-channel flow (Manning)
Answer: Q = 15.94 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 = 3·2.1 = 6.3 m²
P = b + 2y = 3 + 2·2.1 = 7.2 m
R = A/P = 0.875 m
Velocity
V = (1/0.014)·0.8752/3·0.00151/2 = 2.531 m/s
Flow rate
Q = A·V = 6.3·2.531 = 15.94 m³/s
Answer
Q = 15.94 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.00105 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 = (5.5 + 1·1.6)·1.6 = 11.36 m²
P = b + 2y·√(1 + z²) = 5.5 + 2·1.6·√(1 + 1²) = 10.03 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.
Hydraulic power
Ph = ρ·g·Q·H = 1000·9.81·0.01·20 = 1.962 kW
Shaft power
Pshaft = Ph/η = 1.962/0.8 = 2.453 kW
Answer
Pshaft = 2.453 kW
24.Pumps & pump power
Answer: H = 29.94 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.
Both surfaces are open and practically at rest, so pressure and velocity terms drop out.
H = Δz + hL = 16 + 13.94 = 29.94 m
Answer
H = 29.94 m
25.Time value of money
Answer: FV = 26664 €
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.
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.
Whatever is still owed must be exactly paid off by the remaining payments.
N − k = 360 − 228 = 132
B = 1123·(1 − (1 + 0.0045)−132)/0.0045 = €111 594.74
Answer
B = €111 594.74
27.NPV & IRR
Answer: NPV = −1523 €
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 + 0.1)1 = 15 000/1.1 = 13 636.36
CF2/(1 + 0.1)2 = 9 000/1.21 = 7 438.02
CF3/(1 + 0.1)3 = 18 000/1.331 = 13 523.67
CF4/(1 + 0.1)4 = 13 000/1.464 = 8 879.17
Add them up
NPV = €−1 522.78
Answer
NPV = €−1 522.78
NPV is negative, so the project earns less than the required return.
28.NPV & IRR
Answer: IRR = 27.4 %
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(25%) = 1 312.00
NPV(30%) = −1 342.74
Narrow down
Linear interpolation gives a first estimate; repeating it (or a calculator's IRR function) gives the exact rate.
Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.
z-scores
z₁ = (57 − 65)/10 = −0.8
z₂ = (85 − 65)/10 = 2
Area between
P = Φ(2) − Φ(−0.8) = 0.9772 − 0.2119 = 0.7654
Answer
P = 0.7654
30.Normal distribution
Answer: x = 245.8 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) = 0.2 → z = −0.8416
Back to x
x = 250 + −0.8416·5 = 245.79 g
Answer
x = 245.79 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.