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 cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w from the wall to 3 m and a point load P at 1.5 m from the wall. Find the magnitude of the reaction moment MA at the wall.
L = 4 mP = 10 kN at 1.5 mw = 10 kN/m from 0 to 3 m
MA = kN·m
2.Beam support reactionsHard
The simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RA.
L = 10 mP = 10 kN at 2 mw = 6 kN/m from 2 to 10 m
RA = 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 = 5 mheight = 2 mB is 3 m from Avertical load = 25 kN
FAB = kN
4.Truss: method of jointsHard
Use the method of joints to find the force FBC in member BC. Give tension as positive and compression as negative.
span = 8 mheight = 4 mB is 7 m from Avertical load = 20 kNhorizontal load = 20 kN ←
FBC = kN
5.Shear force & bending momentMedium
Find the bending moment Mx at the section x = 2.5 m from support A. Use sagging moments positive and upward shear on the left face positive.
L = 4 mw = 5 kN/m from 0 to 4 mx = 2.5 m
Mx = kN·m
6.Shear force & bending momentHard
The simply supported beam carries a uniformly distributed load w over its whole span and a point load P. Find the maximum bending moment Mmax in the beam.
L = 8 mP = 25 kN at 7 mw = 4 kN/m from 0 to 8 m
Mmax = 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 = 10 kN/mL = 3 mE = 70 GPa (aluminium)I = 36 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
A simply supported beam carries a uniformly distributed load w. Its deflection may not exceed span/360. Find the smallest second moment of area Ireq that meets this limit.
w = 10 kN/mL = 5 mE = 70 GPa (aluminium)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
A column of length L made of steel is pinned at both ends. Using Euler’s formula, find its critical buckling load Pcr.
L = 2 mE = 200 GPa (steel)b × h = 30 × 80 mm
Pcr = kN
10.Column bucklingHard
A solid round column of length L made of steel is fixed at the base and free at the top. It must carry 90 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.
P = 90 kNn = 2L = 5 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
A circular tube has outside diameter D = 260 mm and inside diameter d = 240 mm. Find its radius of gyration r about the horizontal centroidal axis.
D = 260 mmd = 240 mm
r = mm
12.Centroid & second moment of areaHard
The T-section is used as a beam with the flange on top and carries a sagging bending moment of 15 kN·m. Find the bending stress σbottom at the bottom edge.
A 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 50 kPa and the preconsolidation pressure is 100 kPa. A new building adds 150 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.
A clay layer 4 m thick has a coefficient of consolidation cv = 0.8 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 70% average consolidation the time factor is Tv = 0.403. How many years t does the layer take to reach 70% consolidation?
A vertical rectangular gate 1 m wide sits in the wall of a tank of water, with its top edge 1 m below the surface. Find the resultant hydrostatic force F on the gate.
d = 1 mH = 2 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
A vertical rectangular gate 3 m wide sits in the wall of a tank of seawater, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.
Water flows at a mean velocity of 1.7 m/s through a pipe 800 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.
A pipe 300 m long with an inside diameter of 200 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), 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 100 L/s?
A concrete storm sewer with an inside diameter of 300 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.0015. Find the flow rate Q in m³/s.
D = 300 mmn = 0.013S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
A rectangular finished concrete channel 1.5 m wide must carry 2.4 m³/s in uniform flow at a depth of 0.9 m. Manning n = 0.012. Find the required bed slope S (in m/m).
Q = 2.4 m³/sb = 1.5 my = 0.9 mn = 0.012
S = m/m
23.Pumps & pump powerMedium
A pump with an efficiency of 70% delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 76 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.
Q = 60 L/sH = 76 mη = 70%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
A pump moves 60 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 6 m higher. The pipe is 300 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 4 (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.
You need €10 000 in 8 years. An account pays 5% per year, compounded quarterly. How much must you deposit today? Find the present value PV.
FV = €10 0005% / 4n = 8
PV = €
26.Time value of moneyHard
You want €100 000 in 11 years. You save the same amount at the end of every month in an account paying 6% per year, compounded monthly. Find the monthly deposit A.
FV = €100 0006% / 12N = 132
A = €
27.NPV & IRRMedium
An investment of €60 000 gives these cash flows at the end of years 1 to 4: €16 000, €26 000, €14 000, €21 000. The cost of capital is 9%. Find the net present value NPV.
An investment of €10 000 returns €2 000 at the end of each year for 8 years. Find its internal rate of return IRR in percent.
C0 = €10 000CF = €2 000n = 8
IRR = %
29.Normal distributionMedium
X is normal with mean 12 min and standard deviation 1.5 min; Y is independent and normal with mean 20 min and standard deviation 2 min. Find the probability P that X + Y is more than 33.3 min. Round z to two decimals.
μX = 12, σX = 1.5μY = 20, σY = 2X + Y > 33.3 min
P =
30.Normal distributionHard
The bag weights are normally distributed with mean 250 g and standard deviation 5 g. Drag the cut-off so the shaded top 30% is to the right of it. Find the cut-off x.
μ = 250 gσ = 5 g30%
x = g
3Solutions
1.Beam support reactions
Answer: MA = 60 kN·m
Cantilever equilibrium: a fixed support can push up and also resist rotation, so it gives a vertical reaction RA and a reaction moment MA. ΣFy = 0 gives RA, and moments about the wall give MA = Σ(load × distance from the wall). A distributed load acts as its resultant at the centroid of the load diagram.
Resultant of the distributed load
W = 10·3 = 30 kN, x̄ = 1.5 m
Moment about the wall
MA = P·a + W·x̄ = 10·1.5 + 30·1.5 = 60 kN·m
Answer
MA = 60 kN·m
2.Beam support reactions
Answer: RA = 27.2 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 = 6·8 = 48 kN, acting at x̄ = 6 m
ΣMA = 0: RB·10 = 10·2 + 6·8·6
RB = 308/10 = 30.8 kN
ΣFy = 0: RA = 58 − 30.8 = 27.2 kN
Answer
RA = 27.2 kN
3.Truss: method of joints
Answer: FAB = −18.03 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.
Support reactions
Equilibrium of the whole truss. Moments about A, counter-clockwise positive.
ΣMA = 0: Cy·5 = 25·3 → Cy = 15 kN
ΣFy = 0: Ay = 25 − 15 = 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 = 2/3.606 = 0.5547
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −10/0.5547 = −18.03 kN
Answer
FAB = −18.03 kN (compression)
4.Truss: method of joints
Answer: FBC = −7.731 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·8 = 20·7 − 20·4 → Cy = 7.5 kN
ΣFy = 0: Ay = 20 − 7.5 = 12.5 kN
ΣFx = 0: Ax = 20 kN
Joint C
The roller gives only a vertical reaction, so joint C has just two unknown member forces. Assume both in tension.
sin γ = 4/4.123 = 0.9701, cos γ = 1/4.123 = 0.2425
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 = 5·4 = 20 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 5·4·2
RB = 40/4 = 10 kN
ΣFy = 0: RA = 20 − 10 = 10 kN
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.
M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 10·2.5 − 5·2.5·1.25 = 9.375 kN·m
Answer
Mx = 9.375 kN·m
6.Shear force & bending moment
Answer: Mmax = 45.72 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.
UDL resultant: W = w·ℓ = 4·8 = 32 kN, acting at x̄ = 4 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).
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 = 10 N/mm, L = 3000 mm
EI = 2.52 × 10¹² N·mm²
Deflection
δmax = 5wL⁴/(384EI) = 5·10·3000⁴/(384·2.52 × 10¹²) = 4.185 mm
Answer
δmax = 4.185 mm
8.Beam deflection
Answer: Ireq = 83.71 × 10⁶ mm⁴
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).
Deflection limit
δallow = L/360 = 5000/360 = 13.89 mm
Required second moment of area
I = 5wL⁴/(384·E·δallow) = 5·10·5000⁴/(384·70000·13.89) = 8.371 × 10⁷ mm⁴
Ireq = 83.71 × 10⁶ mm⁴
Answer
Ireq = 83.71 × 10⁶ mm⁴
9.Column buckling
Answer: Pcr = 88.83 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.
Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.
Required critical load
Pcr = n·P = 2·90000 = 180000 N
KL = 2·5000 = 10000 mm
Solve for the diameter
d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·180000·10000²/(π³·200000))^(1/4) = 116.7 mm
Answer
d = 116.7 mm
Check: the slenderness KL/r is 342.6, so the column is slender and Euler applies.
11.Centroid & second moment of area
Answer: r = 88.46 mm
Second moment of area: for a rectangle about its own centroidal axis I = bh³/12, and about its base bh³/3 (parallel-axis theorem I = Ic + A·d²). A hole is handled by subtracting its I, as long as both parts share the same axis. The elastic section modulus is S = I/c, where c is the distance to the extreme fibre. The radius of gyration r = √(I/A) is the distance at which the whole area would give the same I; it is used in column buckling.
Net area and second moment of area
A = π(D² − d²)/4 = 7854 mm²
I = π(D⁴ − d⁴)/64 = 6.146 × 10⁷ mm⁴
Radius of gyration
r = √(I/A) = √(6.146 × 10⁷/7854) = 88.46 mm
Answer
r = 88.46 mm
12.Centroid & second moment of area
Answer: σbottom = 41.5 MPa
Composite areas: split the section into rectangles. The centroid is the area-weighted average ȳ = ΣAᵢyᵢ/ΣAᵢ. The second moment of area about the centroidal axis adds each part’s own bh³/12 and its parallel-axis term A·d², where d is the distance from the part’s centroid to the overall centroid. Bending stress is σ = M·y/I.
Split into two rectangles
Measure every y from the bottom edge.
flange: Af = 100·25 = 2500 mm², yf = 260 + 25/2 = 272.5 mm
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.
Water pressure grows with depth below the water table.
u = γw·(z − zw) = 9.81·2 = 19.62 kPa
Effective stress
σ′ = σ − u = 56.5 − 19.62 = 36.88 kPa
Answer
σ′ = 36.88 kPa
14.Effective stress in soil
Answer: u = 39.24 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).
Pore water pressure
Water pressure grows with depth below the water table.
u = γw·(z − zw) = 9.81·4 = 39.24 kPa
Answer
u = 39.24 kPa
15.Consolidation settlement
Answer: S = 366.9 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 = 50 + 150 = 200 kPa > 100 kPa
Settlement
Recompression up to σ′p, virgin compression beyond it.
S = 0.04·5/(1 + 0.6)·log₁₀(100/50) + 0.35·5/(1 + 0.6)·log₁₀(200/100)
S = 37.63 + 329.3 = 366.9 mm
Answer
S = 366.9 mm
16.Consolidation settlement
Answer: t = 2.015 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 = 4/2 = 2 m
Time
t = Tv·Hdr²/cv = 0.403·2²/0.8 = 2.015 years
Answer
t = 2.015 years
17.Hydrostatic force
Answer: F = 39.24 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 + 2/2 = 2 m
A = H·b = 2·1 = 2 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·2·2 = 39.24 kN
Answer
F = 39.24 kN
18.Hydrostatic force
Answer: F = 124.4 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 = 1.5·3 = 4.5 m²
Resultant force
F = ρ·g·yc·A = 1025·9.81·2.75·4.5 = 124.4 kN
Answer
F = 124.4 kN
19.Pipe friction & head loss
Answer: hf = 5.892 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 head
V²/(2g) = 1.7²/(2·9.81) = 0.1473 m
Darcy–Weisbach
hf = f·(L/D)·V²/(2g) = 0.015·(800/0.3)·1.7²/(2·9.81) = 5.892 m
Answer
hf = 5.892 m
20.Pipe friction & head loss
Answer: H = 22.05 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 = 0.1/0.03142 = 3.183 m/s
V²/(2g) = 0.5164 m
Loss coefficients
f·L/D = 0.02·300/0.2 = 30
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 + 30 + 11.7)·0.5164 = 22.05 m
Answer
H = 22.05 m
21.Open-channel flow (Manning)
Answer: Q = 0.03745 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 = 0.07069 m², R = D/4 = 0.075 m
Velocity
V = (1/0.013)·0.0752/3·0.00151/2 = 0.5298 m/s
Flow rate
Q = A·V = 0.07069·0.5298 = 0.03745 m³/s
Answer
Q = 0.03745 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.001499 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.
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 = 1000·9.81·0.06·76 = 44.73 kW
Shaft power
Pshaft = Ph/η = 44.73/0.7 = 63.91 kW
Answer
Pshaft = 63.91 kW
24.Pumps & pump power
Answer: H = 32.15 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 practically at rest, so there is no velocity head term.
H = Δz + p/(ρ·g) + hL = 6 + 20.39 + 5.763 = 32.15 m
Answer
H = 32.15 m
25.Time value of money
Answer: PV = 6720 €
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 = 0.05/4 = 0.0125
N = 4·8 = 32
Present value
PV = FV/(1 + i)N = 10 000/1.488 = €6 719.84
Answer
PV = €6 719.84
26.Time value of money
Answer: A = 536.7 €
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.
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 + 0.09)1 = 16 000/1.09 = 14 678.90
CF2/(1 + 0.09)2 = 26 000/1.188 = 21 883.68
CF3/(1 + 0.09)3 = 14 000/1.295 = 10 810.57
CF4/(1 + 0.09)4 = 21 000/1.412 = 14 876.93
Add them up
NPV = €2 250.08
Answer
NPV = €2 250.08
NPV is positive, so the project earns more than the required return.
28.NPV & IRR
Answer: IRR = 11.81 %
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.
Required annuity factor
(1 − (1 + i)−8)/i = 10 000/2 000 = 5
Solve for the rate
The annuity factor falls as the rate rises; bracket the rate and narrow down.
i = 11%: 5.146
i = 12%: 4.968
IRR = 11.81%
Answer
IRR = 11.81%
29.Normal distribution
Answer: P = 0.3015
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 sum
μ = 32 min, σ = √(1.5² + 2²) = 2.5 min
Standardise
z = (33.3 − 32)/2.5 = 0.52
Upper tail
P = 1 − Φ(0.52) = 1 − 0.6985 = 0.3015
Answer
P = 0.3015
30.Normal distribution
Answer: x = 252.6 g
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
Φ(z) = 0.7
z from the table
z ≈ 0.52
Back to the original units
x = 250 + 0.52·5 = 252.6 g
Answer
x = 252.6 g
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