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 simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RA.
L = 6 mP1 = 40 kN at 1 mP2 = 30 kN at 5 m
RA = 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 = 6 mP = 35 kN at 2 mw = 8 kN/m from 2 to 5 m
RB = kN
3.Truss: method of jointsMedium
Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.
B: 20 kN ↓H: 10 kN ↓
1member AB
2member BC
3member CD
4member DE
5member FG
6member GH
7member AF
8member HE
9member BF
10member CG
11member DH
12member BG
13member DG
4.Truss: method of jointsHard
Use the method of joints to find the force FAB in member AB. Give tension as positive and compression as negative.
span = 8 mheight = 3 mB is 3 m from Avertical load = 40 kNhorizontal load = 10 kN ←
FAB = kN
5.Shear force & bending momentMedium
The simply supported beam carries a clockwise couple M0 = 35 kN·m at x = 7 m from A, and no other load. Find the bending moment Mx just to the left of the couple. Use sagging moments positive and upward shear on the left face positive.
L = 8 mM0 = 35 kN·m clockwise, at 7 m
Mx = kN·m
6.Shear force & bending momentHard
Find the bending moment Mx at the section x = 0.5 m from support A. Use sagging moments positive and upward shear on the left face positive.
L = 8 mP = 60 kN at 4 mw = 2 kN/m from 0 to 8 mx = 0.5 m
Mx = kN·m
7.Beam deflectionMedium
A simply supported beam carries a uniformly distributed load w over its whole span. Find the slope θA of the beam at support A, in radians.
w = 20 kN/mL = 3 mE = 70 GPa (aluminium)I = 23 × 10⁶ mm⁴
θA = rad
8.Beam deflectionHard
A propped cantilever is fixed at A and simply supported (propped) at B. It carries a uniformly distributed load w over its whole length. EI is constant. Find the size of the bending moment MA at the fixed end.
L = 5 mw = 8 kN/m
MA = kN·m
9.Column bucklingMedium
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 = 6 mE = 200 GPa (steel)b × h = 30 × 100 mm
Pcr = kN
10.Column bucklingHard
A column of length L made of steel is fixed at the base and free at the top. Find its slenderness and the critical buckling stress σcr from Euler’s formula.
L = 1 mE = 200 GPa (steel)d = 30 mm
σcr = MPa
11.Centroid & second moment of areaMedium
Find the second moment of area Ix of the T-section about the horizontal axis x through its centroid.
bf = 240 mmtf = 15 mmtw = 16 mmhw = 120 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
A symmetric I-section has flanges 250 mm wide and 18 mm thick, an overall depth of 440 mm and a web 6 mm thick. It carries a bending moment of 120 kN·m about the axis x. Find the size of the bending stress σj at the junction of the web and the top flange.
A 2.5 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.04 and e₀ = 0.6. At its mid-depth the effective vertical stress is 110 kPa and the preconsolidation pressure is 200 kPa. A new building adds 240 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.
A clay layer 9 m thick has a coefficient of consolidation cv = 4 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. 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 = 3 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
A vertical rectangular gate 1 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.
d = 2 mH = 3 mb = 1 mρ = 880 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Water flows at 20 L/s through a pipe 500 m long with an inside diameter of 100 mm. Use the Darcy friction factor f = 0.022 and g = 9.81 m/s². Find the friction head loss hf.
Two open reservoirs are joined by a pipe 200 m long with an inside diameter of 300 mm and a Darcy friction factor f = 0.018. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each), a valve (K = 5) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². What difference in water level Δz between the reservoirs gives a flow rate of 75 L/s?
A trapezoidal finished concrete channel has a bottom width of 3 m and side slopes of 1:1 (horizontal:vertical). Water flows uniformly 1.2 m deep. Manning n = 0.012 and the bed slope is S = 0.0015. Find the flow rate Q in m³/s.
b = 3 my = 1.2 mz = 1n = 0.012S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
A concrete sewer with an inside diameter of 300 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.75 m/s when flowing just full. Find the minimum slope S (in m/m).
D = 300 mmn = 0.013V = 0.75 m/s
S = m/m
23.Pumps & pump powerMedium
A pump delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 56 m. The pump efficiency is 85% and the electric motor driving it has an efficiency of 92%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.
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 34 m higher. The pipe is 200 m long with an inside diameter of 250 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.
An annuity pays €3 000 at the end of each year for 14 years. The interest rate is 8% per year. Find the present value PV of the annuity.
A = €3 000i = 8%n = 14
PV = €
26.Time value of moneyHard
A mortgage of €200 000 is repaid with equal monthly payments over 25 years at 3.6% per year, compounded monthly. How much is still owed just after the payment at the end of year 17? Find the outstanding balance B.
P = €200 0003.6% / 12N = 300k = 204
B = €
27.NPV & IRRMedium
An investment of €60 000 gives these cash flows at the end of years 1 to 4: €14 000, €28 000, €13 000, €19 000. The cost of capital is 6%. Find the net present value NPV.
A project costs €25 000 and returns €12 000, €15 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.
CF0 = −25 000CF1 = 12 000CF2 = 15 000
IRR = %
29.Normal distributionMedium
Drag z so that the shaded area between −z and z under the standard normal curve is 0.6102. Find z to two decimals.
A = 0.6102
z =
30.Normal distributionHard
The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. Find the value x below which 5% of them lie (the 5th percentile).
μ = 500σ = 40P = 5%
x = h
3Solutions
1.Beam support reactions
Answer: RA = 38.33 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.
ΣMA = 0: RB·6 = 40·1 + 30·5
RB = 190/6 = 31.67 kN
ΣFy = 0: RA = 70 − 31.67 = 38.33 kN
Answer
RA = 38.33 kN
2.Beam support reactions
Answer: RB = 25.67 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 = 8·3 = 24 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·6 = 35·2 + 8·3·3.5
RB = 154/6 = 25.67 kN
ΣFy = 0: RA = 59 − 25.67 = 33.33 kN
Answer
RB = 25.67 kN
3.Truss: method of joints
Answer: member CG
Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.
Joint C
BC and CD lie on one straight line and the joint carries no load. Balancing forces across that line leaves only CG.
ΣF⊥ = 0 → FCG = 0
Check with the method of joints
Solving all joints gives these member forces (T = tension, C = compression).
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·8 = 40·3 − 10·3 → Cy = 11.25 kN
ΣFy = 0: Ay = 40 − 11.25 = 28.75 kN
ΣFx = 0: Ax = 10 kN
Joint A
Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.
sin α = 3/4.243 = 0.7071
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −28.75/0.7071 = −40.66 kN
Answer
FAB = −40.66 kN (compression)
5.Shear force & bending moment
Answer: Mx = −30.63 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. An applied couple makes the bending moment diagram jump by the size of the couple.
Support reactions
Moments about A, counter-clockwise positive: RB·L − M0 = 0. Vertical balance: RA + RB = 0.
RB = M0/L = 35/8 = 4.375 kN (upward)
RA = −RB = −4.375 kN (downward)
Cut just left of the couple
The left part contains only RA.
Mx = RA·a = −4.375·7 = −30.63 kN·m
Answer
Mx = −30.63 kN·m
6.Shear force & bending moment
Answer: Mx = 18.75 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 = 2·8 = 16 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 60·4 + 2·8·4
RB = 304/8 = 38 kN
ΣFy = 0: RA = 76 − 38 = 38 kN
Cut at x = 0.5 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.
M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 38·0.5 − 2·0.5·0.25 = 18.75 kN·m
Answer
Mx = 18.75 kN·m
7.Beam deflection
Answer: θA = 0.01398 rad
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). The slope θ = dv/dx is the first integral of M/(EI); in consistent units it comes out in radians.
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 = 20 N/mm, L = 3000 mm
EI = 1.61 × 10¹² N·mm²
End slope
θA = wL³/(24EI) = 20·3000³/(24·1.61 × 10¹²) = 0.01398 rad
Answer
θA = 0.01398 rad
That is 0.8007°.
8.Beam deflection
Answer: MA = 25 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 = wL⁴/(8EI)
Compatibility at the prop
The prop force RB alone lifts the free end by RBL³/(3EI). The prop holds B at zero deflection, so the two must cancel. EI cancels out.
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.
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 = 2·1000 = 2000 mm
KL/r = 2000/7.5 = 266.7
Critical stress
σcr = π²E/(KL/r)² = π²·200000/266.7² = 27.76 MPa
Answer
σcr = 27.76 MPa
11.Centroid & second moment of area
Answer: Ix = 8.077 × 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 = 240·15 = 3600 mm², yf = 120 + 15/2 = 127.5 mm
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.
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).
Total stress
Add the weight of each soil band above X. Above the water table use the dry unit weight, below it the saturated one.
σ = γd·1 + γsat,sand·2 + γsat,clay·2
σ = 15.5·1 + 18.5·2 + 18.5·2 = 89.5 kPa
Answer
σ = 89.5 kPa
15.Consolidation settlement
Answer: S = 149.1 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 = 110 + 240 = 350 kPa > 200 kPa
Settlement
Recompression up to σ′p, virgin compression beyond it.
S = 0.04·2.5/(1 + 0.6)·log₁₀(200/110) + 0.35·2.5/(1 + 0.6)·log₁₀(350/200)
S = 16.23 + 132.9 = 149.1 mm
Answer
S = 149.1 mm
16.Consolidation settlement
Answer: t = 17.17 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 = 9 m
Time
t = Tv·Hdr²/cv = 0.848·9²/4 = 17.17 years
Answer
t = 17.17 years
17.Hydrostatic force
Answer: F = 309 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 = 3·3 = 9 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·3.5·9 = 309 kN
Answer
F = 309 kN
18.Hydrostatic force
Answer: F = 90.64 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 = 3 m²
Resultant force
F = ρ·g·yc·A = 880·9.81·3.5·3 = 90.64 kN
Answer
F = 90.64 kN
19.Pipe friction & head loss
Answer: hf = 36.36 m
Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.
Mean velocity
A = π·0.1²/4 = 0.007854 m²
V = Q/A = 0.02/0.007854 = 2.546 m/s
Velocity head
V²/(2g) = 2.546²/(2·9.81) = 0.3305 m
Darcy–Weisbach
hf = f·(L/D)·V²/(2g) = 0.022·(500/0.1)·2.546²/(2·9.81) = 36.36 m
Answer
hf = 36.36 m
20.Pipe friction & head loss
Answer: Δz = 1.13 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 = 0.075/0.07069 = 1.061 m/s
V²/(2g) = 0.05738 m
Loss coefficients
f·L/D = 0.018·200/0.3 = 12
ΣK = 0.5 + 4·0.3 + 5 + 1.0 = 7.7
Total head loss
hf = 12·0.05738 = 0.6886 m
hm = 7.7·0.05738 = 0.4418 m
Δz = hf + hm = 1.13 m
Answer
Δz = 1.13 m
21.Open-channel flow (Manning)
Answer: Q = 13.88 m³/s
Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.
Geometry
A = (b + z·y)·y = (3 + 1·1.2)·1.2 = 5.04 m²
P = b + 2y·√(1 + z²) = 3 + 2·1.2·√(1 + 1²) = 6.394 m
R = A/P = 0.7882 m
Velocity
V = (1/0.012)·0.78822/3·0.00151/2 = 2.754 m/s
Flow rate
Q = A·V = 5.04·2.754 = 13.88 m³/s
Answer
Q = 13.88 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.003006 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 = 0.3/4 = 0.075 m
Solve Manning for S
S = (n·V/R2/3)² = (0.013·0.75/0.1778)² = 0.003006
Answer
S = 0.003006
That is a fall of 3.006 m per kilometre.
23.Pumps & pump power
Answer: Pel = 42.15 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 = 1000·9.81·0.06·56 = 32.96 kW
Shaft power
Pshaft = 32.96/0.85 = 38.78 kW
Electrical power
Pel = 38.78/0.92 = 42.15 kW
Answer
Pel = 42.15 kW
24.Pumps & pump power
Answer: H = 41.31 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 = 34 + 7.31 = 41.31 m
Answer
H = 41.31 m
25.Time value of money
Answer: PV = 24733 €
Time value of money: money today is worth more than the same amount later, because it can earn interest. With interest rate i per period, an amount grows as FV = PV·(1 + i)n. A series of equal payments (an annuity) is valued by adding up each payment, which gives the annuity formulas.
Annuity factor
(1 − (1 + i)−n)/i = (1 − 0.3405)/0.08 = 8.244
Present value
PV = 3 000·8.244 = €24 732.71
Answer
PV = €24 732.71
26.Time value of money
Answer: B = 84305 €
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 = 300 − 204 = 96
B = 1012·(1 − (1 + 0.003)−96)/0.003 = €84 305.14
Answer
B = €84 305.14
27.NPV & IRR
Answer: NPV = 4092 €
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 = −60 000
CF1/(1 + 0.06)1 = 14 000/1.06 = 13 207.55
CF2/(1 + 0.06)2 = 28 000/1.124 = 24 919.90
CF3/(1 + 0.06)3 = 13 000/1.191 = 10 915.05
CF4/(1 + 0.06)4 = 19 000/1.262 = 15 049.78
Add them up
NPV = €4 092.28
Answer
NPV = €4 092.28
NPV is positive, so the project earns more than the required return.
28.NPV & IRR
Answer: IRR = 5.093 %
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(5%) = 34.01
NPV(10%) = −1 694.21
Narrow down
Linear interpolation gives a first estimate; repeating it (or a calculator's IRR function) gives the exact rate.
IRR ≈ 5 + 5·34.01/(34.01 − (−1 694.21)) = 5.098%
exact: NPV(5.093%) = 0 → IRR = 5.093%
Answer
IRR = 5.093%
29.Normal distribution
Answer: z = 0.86
From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.
Area to the left of z
Φ(z) = (1 + 0.6102)/2 = 0.8051
Read the z-table backwards
Find 0.8051 inside the table and read off z.
z = 0.86
Answer
z = 0.86
30.Normal distribution
Answer: x = 434.2 h
Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.
z for the percentile
Φ(z) = 0.05 → z = −1.645
Back to x
x = 500 + −1.645·40 = 434.2 h
Answer
x = 434.2 h
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