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 = 4 mP1 = 25 kN at 2 mP2 = 25 kN at 2.5 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 RA.
L = 8 mP = 40 kN at 2 mw = 10 kN/m from 2 to 5 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 = 3 mB is 3 m from Avertical load = 60 kN
FAB = kN
4.Truss: method of jointsHard
Use the method of joints to find the force FAC in member AC. Give tension as positive and compression as negative.
span = 8 mheight = 3 mB is 6 m from Avertical load = 15 kNhorizontal load = 5 kN →
FAC = kN
5.Shear force & bending momentMedium
The marks A to G split the beam into six equal parts. At which mark is the bending moment largest in size, sagging or hogging? Click it in the diagram.
20 kN @ 3 m5 kN/m, 0–6 m
1A (x = 0 m)
2B (x = 1 m)
3C (x = 2 m)
4D (x = 3 m)
5E (x = 4 m)
6F (x = 5 m)
7G (x = 6 m)
6.Shear force & bending momentHard
The marks A to G split the beam into six equal parts. At which mark is the bending moment largest in size, sagging or hogging? Click it in the diagram.
35 kN @ 12 m55 kN @ 4 m8 kN/m, 0–8 m
1A (x = 0 m)
2B (x = 2 m)
3C (x = 4 m)
4D (x = 6 m)
5E (x = 8 m)
6F (x = 10 m)
7G (x = 12 m)
7.Beam deflectionMedium
A cantilever of length L is fixed at A and carries a point load P at a distance a = 1 m from A. Find the deflection δB at the free end B.
P = 24 kNa = 1 mL = 2 mE = 70 GPa (aluminium)I = 57 × 10⁶ mm⁴
δB = mm
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 reaction RB at the prop.
L = 6 mw = 4 kN/m
RB = kN
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 = 3 mE = 200 GPa (steel)b × h = 20 × 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 85 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.
P = 85 kNn = 3L = 2 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
A channel section lies with its open side up: a base plate 200 mm wide with two upright legs, 120 mm high overall. Base and legs are all 10 mm thick. Find the height ȳ of the centroid above the bottom edge.
b = 200 mmh = 120 mmt = 10 mm
ȳ = 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 size of the bending stress σtop at the top edge.
A 4 m thick overconsolidated clay layer has Cc = 0.2, Cr = 0.02 and e₀ = 0.95. At its mid-depth the effective vertical stress is 95 kPa and the preconsolidation pressure is 195 kPa. A new building adds 200 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 = 0.8 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 1.5 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.
A vertical rectangular gate 2 m wide sits in the wall of a tank of oil, with its top edge 4 m below the surface. Find the depth ycp of the centre of pressure below the surface.
d = 4 mH = 2.5 mb = 2 mρ = 880 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
Water (ρ = 1000 kg/m³) flows at 1.1 m/s through a horizontal pipe, 100 m long, with an inside diameter of 75 mm. Use the Darcy friction factor f = 0.025 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 300 mm (Darcy friction factor f = 0.015) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 2 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 80 L/s?
A trapezoidal brickwork channel has a bottom width of 5 m and side slopes of 1:1 (horizontal:vertical). Water flows uniformly 0.6 m deep. Manning n = 0.015 and the bed slope is S = 0.0005. Find the flow rate Q in m³/s.
b = 5 my = 0.6 mz = 1n = 0.015S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
A trapezoidal finished concrete channel with a bottom width of 6 m and side slopes of 1.5:1 (horizontal:vertical) must carry 43 m³/s in uniform flow at a depth of 1.7 m. Manning n = 0.012. Find the required bed slope S (in m/m).
Q = 43 m³/sb = 6 my = 1.7 mz = 1.5n = 0.012
S = m/m
23.Pumps & pump powerMedium
A pump with an efficiency of 75% delivers 60 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 = 60 L/sH = 20 mη = 75%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 150 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 82%. Find the shaft power Pshaft in kW.
A property is expected to earn net rent of €6 000 next year. The rent is expected to grow by 2% per year forever. The required return is 4% per year. Find the value PV of the property today.
C1 = €6 000g = 2%r = 4%
PV = €
26.Time value of moneyHard
You save €200 at the end of every month for 8 years. The account pays 3.6% per year, compounded monthly. How much have you saved at the end? Find FV.
A = €2003.6% / 12N = 96
FV = €
27.NPV & IRRMedium
An investment of €75 000 gives these cash flows at the end of years 1 to 4: €17 000, €24 000, €18 000, €23 000. The cost of capital is 6%. Find the net present value NPV.
A project costs €50 000 and returns €31 000, €24 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.
CF0 = −50 000CF1 = 31 000CF2 = 24 000
IRR = %
29.Normal distributionMedium
The bag weights are normally distributed with mean 250 g and standard deviation 5 g. What fraction lies between 242.75 and 260.25 g? Give P as a decimal.
μ = 250σ = 5x1 = 242.75x2 = 260.25
P =
30.Normal distributionHard
The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Drag the cut-off so the shaded bottom 5% is to the left of it. Find the cut-off x.
μ = 65 pointsσ = 10 points5%
x = points
3Solutions
1.Beam support reactions
Answer: RA = 21.88 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 = 25·2 + 25·2.5
RB = 112.5/4 = 28.13 kN
ΣFy = 0: RA = 50 − 28.13 = 21.88 kN
Answer
RA = 21.88 kN
2.Beam support reactions
Answer: RA = 46.88 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 = 10·3 = 30 kN, acting at x̄ = 3.5 m
ΣMA = 0: RB·8 = 40·2 + 10·3·3.5
RB = 185/8 = 23.13 kN
ΣFy = 0: RA = 70 − 23.13 = 46.88 kN
Answer
RA = 46.88 kN
3.Truss: method of joints
Answer: FAB = −33.94 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 = 60·3 → Cy = 36 kN
ΣFy = 0: Ay = 60 − 36 = 24 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 = −24/0.7071 = −33.94 kN
Answer
FAB = −33.94 kN (compression)
4.Truss: method of joints
Answer: FAC = 8.75 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 = 15·6 + 5·3 → Cy = 13.13 kN
ΣFy = 0: Ay = 15 − 13.13 = 1.875 kN
ΣFx = 0: Ax = −5 kN
Joint C
The roller gives only a vertical reaction, so joint C has just two unknown member forces. Assume both in tension.
sin γ = 3/3.606 = 0.8321, cos γ = 2/3.606 = 0.5547
Largest bending moment: M changes slope wherever the shear force changes, so its peaks sit where the shear force crosses zero: under a point load, inside a distributed load, or over a support of an overhang. At a fixed support of a cantilever the moment is largest at the wall. Compare the size of M at those places, sagging or hogging.
Support reactions
Take moments about one support, then use the vertical force balance.
R1 = 25 kN, R2 = 25 kN
Bending moment at every mark
Sum the moments of all forces on one side of the cut. Sagging is positive, hogging negative.
MA = 0, MB = 22.5, MC = 40, MD = 52.5 kN·m, ME = 40, MF = 22.5, MG = 0
Answer
Mark D: MD = 52.5 kN·m
6.Shear force & bending moment
Answer: E (x = 8 m)
Largest bending moment: M changes slope wherever the shear force changes, so its peaks sit where the shear force crosses zero: under a point load, inside a distributed load, or over a support of an overhang. At a fixed support of a cantilever the moment is largest at the wall. Compare the size of M at those places, sagging or hogging.
Support reactions
Take moments about one support, then use the vertical force balance.
R1 = 42 kN, R2 = 112 kN
Bending moment at every mark
Sum the moments of all forces on one side of the cut. Sagging is positive, hogging negative.
MA = 0, MB = 68, MC = 104, MD = −2, ME = −140 kN·m, MF = −70, MG = 0
Answer
Mark E: ME = −140 kN·m
7.Beam deflection
Answer: δB = 5.013 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 = 24000 N, a = 1000 mm, L = 2000 mm
EI = 3.99 × 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) = 2.005 mm
θP = Pa²/(2EI) = 0.003008 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 5.013 mm
Answer
δB = 5.013 mm
8.Beam deflection
Answer: RB = 9 kN
Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition). For a statically indeterminate beam, remove a redundant support and require the deflection there to be zero (compatibility).
Remove the prop
Without the prop the beam is a cantilever. Its free end would deflect under the load.
δload = 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.
Required critical load
Pcr = n·P = 3·85000 = 255000 N
KL = 0.7·2000 = 1400 mm
Solve for the diameter
d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·255000·1400²/(π³·200000))^(1/4) = 47.66 mm
Answer
d = 47.66 mm
Check: the slenderness KL/r is 117.5, so the column is slender and Euler applies.
11.Centroid & second moment of area
Answer: ȳ = 36.43 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.
Split into rectangles
Take the base at full width and the two legs above it (height h − t), so nothing is counted twice.
base: A1 = 200·10 = 2000 mm², y1 = 5 mm
two legs: A2 = 2·10·110 = 2200 mm², y2 = 10 + 110/2 = 65 mm
Centroid
ȳ = (2000·5 + 2200·65)/4200 = 36.43 mm
Answer
ȳ = 36.43 mm
12.Centroid & second moment of area
Answer: σtop = 37.92 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 = 240·20 = 4800 mm², yf = 140 + 20/2 = 150 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) = 9.81·11 = 107.9 kPa
Effective stress
σ′ = σ − u = 236 − 107.9 = 128.1 kPa
Answer
σ′ = 128.1 kPa
14.Effective stress in soil
Answer: σ′ = 71.85 kPa
Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).
Total stress
Add the weight of each soil band above X. Above the water table use the dry unit weight, below it the saturated one.
σ = γd·2 + γsat,sand·2 + γsat,clay·2.5
σ = 15.5·2 + 20·2 + 18·2.5 = 116 kPa
Pore water pressure
Water pressure grows with depth below the water table.
u = γw·(z − zw) = 9.81·4.5 = 44.15 kPa
Effective stress
σ′ = σ − u = 116 − 44.15 = 71.85 kPa
Answer
σ′ = 71.85 kPa
15.Consolidation settlement
Answer: S = 86.57 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 = 95 + 200 = 295 kPa > 195 kPa
Settlement
Recompression up to σ′p, virgin compression beyond it.
S = 0.02·4/(1 + 0.95)·log₁₀(195/95) + 0.2·4/(1 + 0.95)·log₁₀(295/195)
S = 12.81 + 73.76 = 86.57 mm
Answer
S = 86.57 mm
16.Consolidation settlement
Answer: t = 24.63 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 = 0.197·10²/0.8 = 24.63 years
Answer
t = 24.63 years
17.Hydrostatic force
Answer: F = 119.6 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 + 2.5/2 = 3.25 m
A = H·b = 2.5·1.5 = 3.75 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·3.25·3.75 = 119.6 kN
Answer
F = 119.6 kN
18.Hydrostatic force
Answer: ycp = 5.349 m
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 = 4 + 2.5/2 = 5.25 m
A = H·b = 2.5·2 = 5 m²
Resultant force
F = ρ·g·yc·A = 880·9.81·5.25·5 = 226.6 kN
Centre of pressure
Pressure grows with depth, so the resultant acts below the centroid.
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) = 0.025·(100/0.075)·1.1²/(2·9.81) = 2.056 m
Pressure drop
The pipe is horizontal and the velocity does not change, so the energy equation reduces to Δp = ρ·g·hf.
Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.
Velocity
V = Q/A = 0.08/0.07069 = 1.132 m/s
V²/(2g) = 0.06529 m
Loss coefficients
f·L/D = 0.015·200/0.3 = 10
ΣK = 0.5 + 2·0.3 + 2 = 3.1
Energy equation
The outlet jet still carries its velocity head; it is not a loss but it has to be supplied.
H = (1 + 10 + 3.1)·0.06529 = 0.9205 m
Answer
H = 0.9205 m
21.Open-channel flow (Manning)
Answer: Q = 3.163 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 = (5 + 1·0.6)·0.6 = 3.36 m²
P = b + 2y·√(1 + z²) = 5 + 2·0.6·√(1 + 1²) = 6.697 m
R = A/P = 0.5017 m
Velocity
V = (1/0.015)·0.50172/3·0.00051/2 = 0.9412 m/s
Flow rate
Q = A·V = 3.36·0.9412 = 3.163 m³/s
Answer
Q = 3.163 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.0009902 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 = (6 + 1.5·1.7)·1.7 = 14.54 m²
P = b + 2y·√(1 + z²) = 6 + 2·1.7·√(1 + 1.5²) = 12.13 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 = 1000·9.81·0.06·20 = 11.77 kW
Shaft power
Pshaft = Ph/η = 11.77/0.75 = 15.7 kW
Answer
Pshaft = 15.7 kW
24.Pumps & pump power
Answer: Pshaft = 20.74 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.
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 €19 200 yourself; the rest is interest.
27.NPV & IRR
Answer: NPV = −4271 €
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 = −75 000
CF1/(1 + 0.06)1 = 17 000/1.06 = 16 037.74
CF2/(1 + 0.06)2 = 24 000/1.124 = 21 359.91
CF3/(1 + 0.06)3 = 18 000/1.191 = 15 113.15
CF4/(1 + 0.06)4 = 23 000/1.262 = 18 218.15
Add them up
NPV = €−4 271.05
Answer
NPV = €−4 271.05
NPV is negative, so the project earns less than the required return.
28.NPV & IRR
Answer: IRR = 6.901 %
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%) = 1 292.52
NPV(10%) = −1 983.47
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.
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) = 0.05
z from the table
z ≈ −1.64
Back to the original units
x = 65 − 1.64·10 = 48.6 points
Answer
x = 48.6 points
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