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 RB.
L = 4 mP1 = 45 kN at 2.5 mP2 = 40 kN at 3 m
RB = kN
2.Beam support reactionsHard
The beam has a pin at A and a roller at B, 2.5 m from A, and overhangs B to the free end C. It carries a point load P at 0.5 m from A and a uniformly distributed load w from 2 m to the free end at 4 m. Find the vertical reaction RB, taking upward as positive.
AB = 2.5 mAC = 4 mP = 40 kN at 0.5 mw = 5 kN/m from 2 to 4 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: 30 kN ↓D: 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
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.
The cantilever is fixed at A. It carries a uniformly distributed load w over its whole length and a point load P at 1.5 m from A. Find the bending moment MA at the fixed support A. Use sagging moments positive and upward shear on the left face positive.
L = 3 mP = 35 kN at 1.5 mw = 4 kN/m from 0 to 3 m
MA = 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 = 6 mP = 55 kN at 2.5 mw = 10 kN/m from 0 to 6 mx = 0.5 m
Mx = kN·m
7.Beam deflectionMedium
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 = 15 kNa = 1.5 mL = 2 mE = 70 GPa (aluminium)I = 120 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
A simply supported beam carries a uniformly distributed load w and a point load P at midspan. Using superposition, find the midspan deflection δmax.
P = 4 kNw = 2 kN/mL = 6 mE = 11 GPa (timber)I = 120 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
A column of length L made of steel is fixed at the base and pinned at the top. Using Euler’s formula, find its critical buckling load Pcr.
L = 3 mE = 200 GPa (steel)d = 40 mm
Pcr = kN
10.Column bucklingHard
A solid round column of length L made of aluminium is fixed at the base and pinned at the top. It must carry 10 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.
P = 10 kNn = 2L = 1.5 mE = 70 GPa (aluminium)
d = mm
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 = 300 mmtf = 10 mmtw = 10 mmhw = 180 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
A 100 mm × 150 mm plate has a rectangular cut-out 60 mm wide and 40 mm high, centred on the vertical centre line with its centre 97.5 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.
b = 100 mmh = 150 mmcut-out: 60 × 40 mmhole centre: y = 97.5 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
For the soil profile shown, find the vertical effective stress σ′ at point X.
An 8 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.05 and e₀ = 0.85. At its mid-depth the effective vertical stress is 120 kPa and the preconsolidation pressure is 200 kPa. A new building adds 60 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.
A clay layer 10 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 50% average consolidation the time factor is Tv = 0.197. How many years t does the layer take to reach 50% consolidation?
A vertical rectangular gate 2 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.
A vertical rectangular gate 2 m wide sits in the wall of a tank of seawater, with its top edge 2.5 m below the surface. Find the resultant hydrostatic force F on the gate.
Water flows at a mean velocity of 1.8 m/s through a pipe 50 m long with an inside diameter of 50 mm. Use the Darcy friction factor f = 0.028 and g = 9.81 m/s². Find the friction head loss hf.
A pipe 300 m long with an inside diameter of 250 mm (Darcy friction factor f = 0.022) 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 150 L/s?
A concrete storm sewer with an inside diameter of 1200 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.004. Find the flow rate Q in m³/s.
D = 1200 mmn = 0.013S = 0.004
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 1.2 m/s when flowing just full. Find the minimum slope S (in m/m).
D = 300 mmn = 0.013V = 1.2 m/s
S = m/m
23.Pumps & pump powerMedium
A pump with an efficiency of 82% delivers 10 L/s of water (ρ = 1000 kg/m³) against a head of 52 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.
Q = 10 L/sH = 52 mη = 82%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
A pump moves 50 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 150 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 65%. Find the shaft power Pshaft in kW.
You need €40 000 in 8 years. An account pays 3.6% per year, compounded quarterly. How much must you deposit today? Find the present value PV.
FV = €40 0003.6% / 4n = 8
PV = €
26.Time value of moneyHard
You save €50 at the end of every month for 27 years. The account pays 7.2% per year, compounded monthly. How much have you saved at the end? Find FV.
A = €507.2% / 12N = 324
FV = €
27.NPV & IRRMedium
An investment of €20 000 gives these cash flows at the end of years 1 to 3: €10 000, €6 000, €5 000. The cost of capital is 12%. Find the net present value NPV.
A project costs €20 000 and returns €14 000, €14 000, €11 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.
CF0 = −20 000CF1 = 14 000CF2 = 14 000CF3 = 11 000
IRR = %
29.Normal distributionMedium
Drag z so that the shaded area between −z and z under the standard normal curve is 0.6729. Find z to two decimals.
A = 0.6729
z =
30.Normal distributionHard
The heights X of men and Y of women in a group are independent and normal: X has mean 180 cm and standard deviation 10 cm, Y has mean 170 cm and standard deviation 12 cm. Find the probability P that X is greater than Y. Round z to two decimals.
μX = 180 cm, σX = 10 cmμY = 170 cm, σY = 12 cm
P =
3Solutions
1.Beam support reactions
Answer: RB = 58.13 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·4 = 45·2.5 + 40·3
RB = 232.5/4 = 58.13 kN
ΣFy = 0: RA = 85 − 58.13 = 26.88 kN
Answer
RB = 58.13 kN
2.Beam support reactions
Answer: RB = 20 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.
Resultant of the distributed load
W = 5·2 = 10 kN, x̄ = (2 + 4)/2 = 3 m
Equilibrium
Moments about A, counter-clockwise positive. Then vertical force balance.
ΣMA = 0: RB·2.5 = 40·0.5 + 10·3
RB = 50/2.5 = 20 kN
RA = 50 − 20 = 30 kN
Answer
RB = 20 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 G
FG and GH 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).
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 D
CD and DE lie on one straight line and the joint carries no load. Balancing forces across that line leaves only DH.
ΣF⊥ = 0 → FDH = 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.
Keep the free-end part
P: −35·1.5 = −52.5 kN·m
w: −4·3²/2 = −18 kN·m
MA = −52.5 − 18 = −70.5 kN·m
Answer
MA = −70.5 kN·m
Negative means hogging: tension on the top face.
6.Shear force & bending moment
Answer: Mx = 29.79 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 = 10·6 = 60 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 55·2.5 + 10·6·3
RB = 317.5/6 = 52.92 kN
ΣFy = 0: RA = 115 − 52.92 = 62.08 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 = 62.08·0.5 − 10·0.5·0.25 = 29.79 kN·m
Answer
Mx = 29.79 kN·m
7.Beam deflection
Answer: δB = 3.013 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 = 15000 N, a = 1500 mm, L = 2000 mm
EI = 8.4 × 10¹² N·mm²
Deflection at the free end
Deflection at the load plus the slope at the load times the remaining length.
δP = Pa³/(3EI) = 2.009 mm
θP = Pa²/(2EI) = 0.002009 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 3.013 mm
Answer
δB = 3.013 mm
8.Beam deflection
Answer: δmax = 39.2 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 = 4000 N, w = 2 N/mm, L = 6000 mm, EI = 1.32 × 10¹² N·mm²
Each load on its own
δP = PL³/(48EI) = 4000·6000³/(48·1.32 × 10¹²) = 13.64 mm
δw = 5wL⁴/(384EI) = 5·2·6000⁴/(384·1.32 × 10¹²) = 25.57 mm
Add them
δmax = 13.64 + 25.57 = 39.2 mm
Answer
δmax = 39.2 mm
9.Column buckling
Answer: Pcr = 56.25 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.
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 = 2·10000 = 20000 N
KL = 0.7·1500 = 1050 mm
Solve for the diameter
d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·20000·1050²/(π³·70000))^(1/4) = 28.4 mm
Answer
d = 28.4 mm
Check: the slenderness KL/r is 147.9, so the column is slender and Euler applies.
11.Centroid & second moment of area
Answer: Ix = 15.04 × 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 = 300·10 = 3000 mm², yf = 180 + 10/2 = 185 mm
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 = (15000·75 − 2400·97.5)/(15000 − 2400) = 70.71 mm
Full plate about ȳ
100·150³/12 + 15000·4.286² = 28.4 × 10⁶ mm⁴
Hole about ȳ
60·40³/12 + 2400·26.79² = 2.042 × 10⁶ mm⁴
Subtract
Ix = 26.36 × 10⁶ mm⁴
Answer
Ix = 26.36 × 10⁶ mm⁴
13.Effective stress in soil
Answer: σ′ = 135 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.
Water pressure grows with depth below the water table.
u = γw·(z − zw) = 9.81·13 = 127.5 kPa
Effective stress
σ′ = σ − u = 262.5 − 127.5 = 135 kPa
Answer
σ′ = 135 kPa
14.Effective stress in soil
Answer: u = 63.77 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) = 9.81·6.5 = 63.77 kPa
Answer
u = 63.77 kPa
15.Consolidation settlement
Answer: S = 38.07 mm
Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.
Compare with the preconsolidation pressure
σ′f = 120 + 60 = 180 kPa ≤ 200 kPa
Settlement
The clay stays on its recompression line.
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·8/(1 + 0.85)·log₁₀(180/120) = 38.07 mm
Answer
S = 38.07 mm
16.Consolidation settlement
Answer: t = 4.925 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 = 10 m
Time
t = Tv·Hdr²/cv = 0.197·10²/4 = 4.925 years
Answer
t = 4.925 years
17.Hydrostatic force
Answer: F = 80.93 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 = 1.5·2 = 3 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·2.75·3 = 80.93 kN
Answer
F = 80.93 kN
18.Hydrostatic force
Answer: F = 140.8 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 = 2.5 + 2/2 = 3.5 m
A = H·b = 2·2 = 4 m²
Resultant force
F = ρ·g·yc·A = 1025·9.81·3.5·4 = 140.8 kN
Answer
F = 140.8 kN
19.Pipe friction & head loss
Answer: hf = 4.624 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) = 1.8²/(2·9.81) = 0.1651 m
Darcy–Weisbach
hf = f·(L/D)·V²/(2g) = 0.028·(50/0.05)·1.8²/(2·9.81) = 4.624 m
Answer
hf = 4.624 m
20.Pipe friction & head loss
Answer: H = 18.61 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 = 0.15/0.04909 = 3.056 m/s
V²/(2g) = 0.4759 m
Loss coefficients
f·L/D = 0.022·300/0.25 = 26.4
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 + 26.4 + 11.7)·0.4759 = 18.61 m
Answer
H = 18.61 m
21.Open-channel flow (Manning)
Answer: Q = 2.466 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 = 1.131 m², R = D/4 = 0.3 m
Velocity
V = (1/0.013)·0.32/3·0.0041/2 = 2.18 m/s
Flow rate
Q = A·V = 1.131·2.18 = 2.466 m³/s
Answer
Q = 2.466 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.007694 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 = (0.013·1.2/0.1778)² = 0.007694
Answer
S = 0.007694
That is a fall of 7.694 m per kilometre.
23.Pumps & pump power
Answer: Pshaft = 6.221 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 = 1000·9.81·0.01·52 = 5.101 kW
Shaft power
Pshaft = Ph/η = 5.101/0.82 = 6.221 kW
Answer
Pshaft = 6.221 kW
24.Pumps & pump power
Answer: Pshaft = 6.939 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.
Time value of money: money today is worth more than the same amount later, because it can earn interest. With interest rate i per period, an amount grows as FV = PV·(1 + i)n. A series of equal payments (an annuity) is valued by adding up each payment, which gives the annuity formulas.
Rate and number of periods
i = 0.036000000000000004/4 = 0.009
N = 4·8 = 32
Present value
PV = FV/(1 + i)N = 40 000/1.332 = €30 029.12
Answer
PV = €30 029.12
26.Time value of money
Answer: FV = 49551 €
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.
You paid in €16 200 yourself; the rest is interest.
27.NPV & IRR
Answer: NPV = −2729 €
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 = −20 000
CF1/(1 + 0.12)1 = 10 000/1.12 = 8 928.57
CF2/(1 + 0.12)2 = 6 000/1.254 = 4 783.16
CF3/(1 + 0.12)3 = 5 000/1.405 = 3 558.90
Add them up
NPV = €−2 729.36
Answer
NPV = €−2 729.36
NPV is negative, so the project earns less than the required return.
28.NPV & IRR
Answer: IRR = 44.67 %
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(40%) = 1 151.60
NPV(45%) = −77.90
Narrow down
Linear interpolation gives a first estimate; repeating it (or a calculator's IRR function) gives the exact rate.
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 + 0.6729)/2 = 0.8365
Read the z-table backwards
Find 0.8365 inside the table and read off z.
z = 0.98
Answer
z = 0.98
30.Normal distribution
Answer: P = 0.7389
Sums and differences of normal variables: if X and Y are independent and normal, X + Y and X − Y are normal too. Means add or subtract: E(X ± Y) = μX ± μY. Variances always add, also for a difference: Var(X ± Y) = σX² + σY², so σ = √(σX² + σY²). Standard deviations never add directly. The total of n independent items with the same distribution has mean n·μ and standard deviation σ·√n. Then standardise as usual: z = (x − mean)/σ and read Φ(z).
Distribution of the difference
μ = 180 − 170 = 10 cm, σ = 15.62 cm
Standardise
z = (0 − 10)/15.62 = −0.64
Probability
P = 1 − Φ(−0.64) = 0.7389
Answer
P = 0.7389
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