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 = 55 kN at 2 mP2 = 15 kN at 3 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 = 30 kN at 5 mw = 8 kN/m from 5 to 6 m
RA = kN
3.Truss: method of jointsMedium
Use the method of joints to find the force FBC in member BC. Give tension as positive and compression as negative.
span = 5 mheight = 2 mB is 2 m from Avertical load = 55 kN
FBC = 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 = 6 mheight = 3 mB is 1 m from Avertical load = 15 kNhorizontal load = 30 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.
10 kN @ 10 m25 kN @ 6 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)
6.Shear force & bending momentHard
Find the bending moment Mx at the section x = 3 m from support A. Use sagging moments positive and upward shear on the left face positive.
L = 4 mP = 45 kN at 2.5 mw = 3 kN/m from 0 to 4 mx = 3 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 = 2 m from A. Find the deflection δP under the load.
P = 21 kNa = 2 mL = 4 mE = 70 GPa (aluminium)I = 84 × 10⁶ mm⁴
δP = 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 = 5 mE = 70 GPa (aluminium)I = 160 × 10⁶ mm⁴
δmax = mm
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 = 1.5 mE = 200 GPa (steel)b × h = 25 × 60 mm
Pcr = kN
10.Column bucklingHard
A column of length L made of steel is fixed at the base and pinned 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
A channel section lies with its open side up: a base plate 260 mm wide with two upright legs, 90 mm high overall. Base and legs are all 12 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.
b = 260 mmh = 90 mmt = 12 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 60 MPa in tension and 150 MPa in compression. Find the largest hogging bending moment Mallow the beam can carry (give its size).
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 150 kPa. A new building adds 80 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.
A clay layer 5.5 m thick has a coefficient of consolidation cv = 1.5 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 80% average consolidation the time factor is Tv = 0.567. How many years t does the layer take to reach 80% consolidation?
A vertical rectangular gate 1.5 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.
A vertical rectangular gate 1 m wide sits in the wall of a tank of glycerin, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.
Water flows at a mean velocity of 2.2 m/s through a pipe 100 m long with an inside diameter of 200 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 150 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.02. The water surface of the upper reservoir is 5 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each), a valve (K = 2) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². Find the flow rate Q in L/s.
A rectangular grass-lined earth channel is 4 m wide. Water flows uniformly 1.5 m deep. Manning n = 0.03 and the bed slope is S = 0.0005. Find the flow rate Q in m³/s.
b = 4 my = 1.5 mn = 0.03S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
A rectangular finished concrete channel 1.5 m wide must carry 1.3 m³/s in uniform flow at a depth of 0.5 m. Manning n = 0.012. Find the required bed slope S (in m/m).
Q = 1.3 m³/sb = 1.5 my = 0.5 mn = 0.012
S = m/m
23.Pumps & pump powerMedium
A pump with an efficiency of 82% delivers 15 L/s of water (ρ = 1000 kg/m³) against a head of 26 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.
Q = 15 L/sH = 26 mη = 82%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
A pump moves 12 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 100 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 5 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 72%. Find the shaft power Pshaft in kW.
You invest €5 000 at a nominal rate of 4.8% per year, compounded monthly. Find the value FV of the investment after 4 years.
PV = €5 0004.8% / 12n = 4
FV = €
26.Time value of moneyHard
You save €50 at the end of every month for 30 years. The account pays 6% per year, compounded monthly. How much have you saved at the end? Find FV.
A = €506% / 12N = 360
FV = €
27.NPV & IRRMedium
An investment of €30 000 gives these cash flows at the end of years 1 to 4: €12 000, €12 000, €10 000, €14 000. The cost of capital is 8%. Find the net present value NPV.
A project costs €25 000 and returns €11 000, €14 500, €10 000 at the end of years 1 to 3. Cash flows can be reinvested at the cost of capital of 8%. Find the modified internal rate of return MIRR in percent.
The IQ scores are normally distributed with mean 100 points and standard deviation 15 points. What fraction lies between 96.25 and 127 points? Give P as a decimal.
μ = 100σ = 15x1 = 96.25x2 = 127
P =
30.Normal distributionHard
The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Find the value x below which 25% of them lie (the 25th percentile).
μ = 65σ = 10P = 25%
x = points
3Solutions
1.Beam support reactions
Answer: RA = 31.25 kN
Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Taking moments about one support removes that support’s reaction from the equation.
Free-body diagram
Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.
Equilibrium
Moments about A, counter-clockwise positive. Then vertical force balance.
ΣMA = 0: RB·4 = 55·2 + 15·3
RB = 155/4 = 38.75 kN
ΣFy = 0: RA = 70 − 38.75 = 31.25 kN
Answer
RA = 31.25 kN
2.Beam support reactions
Answer: RA = 13.75 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 = 8·1 = 8 kN, acting at x̄ = 5.5 m
ΣMA = 0: RB·8 = 30·5 + 8·1·5.5
RB = 194/8 = 24.25 kN
ΣFy = 0: RA = 38 − 24.25 = 13.75 kN
Answer
RA = 13.75 kN
3.Truss: method of joints
Answer: FBC = −39.66 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 = 55·2 → Cy = 22 kN
ΣFy = 0: Ay = 55 − 22 = 33 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 = 2/3.606 = 0.5547, cos γ = 3/3.606 = 0.8321
Method of joints: every pin of a truss is in equilibrium, so ΣFx = 0 and ΣFy = 0 at each joint. Start at a joint with at most two unknown member forces. A negative result means the member is in compression.
Support reactions
Equilibrium of the whole truss. Moments about A, counter-clockwise positive.
ΣMA = 0: Cy·6 = 15·1 + 30·3 → Cy = 17.5 kN
ΣFy = 0: Ay = 15 − 17.5 = −2.5 kN
ΣFx = 0: Ax = −30 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 = 3/5.831 = 0.5145, cos γ = 5/5.831 = 0.8575
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 = 14.17 kN, R2 = 20.83 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 = 28.33, MC = 56.67, MD = 85 kN·m, ME = 63.33, MF = 41.67, MG = 0
Answer
Mark D: MD = 85 kN·m
6.Shear force & bending moment
Answer: Mx = 32.63 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.
Support reactions
Equilibrium of the whole beam.
UDL resultant: W = w·ℓ = 3·4 = 12 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 45·2.5 + 3·4·2
RB = 136.5/4 = 34.13 kN
ΣFy = 0: RA = 57 − 34.13 = 22.88 kN
Cut at x = 3 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)
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 = 21000 N, a = 2000 mm, L = 4000 mm
EI = 5.88 × 10¹² N·mm²
Deflection under the load
δP = Pa³/(3EI) = 21000·2000³/(3·5.88 × 10¹²) = 9.524 mm
Answer
δP = 9.524 mm
8.Beam deflection
Answer: δmax = 2.383 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 = 5000 mm, EI = 1.12 × 10¹³ N·mm²
Each load on its own
δP = PL³/(48EI) = 4000·5000³/(48·1.12 × 10¹³) = 0.9301 mm
δw = 5wL⁴/(384EI) = 5·2·5000⁴/(384·1.12 × 10¹³) = 1.453 mm
Add them
δmax = 0.9301 + 1.453 = 2.383 mm
Answer
δmax = 2.383 mm
9.Column buckling
Answer: Pcr = 68.54 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.
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 = 0.7·1000 = 700 mm
KL/r = 700/7.5 = 93.33
Critical stress
σcr = π²E/(KL/r)² = π²·200000/93.33² = 226.6 MPa
Answer
σcr = 226.6 MPa
11.Centroid & second moment of area
Answer: Ix = 3.356 × 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 rectangles
Take the base at full width and the two legs above it (height h − t), so nothing is counted twice.
base: A1 = 260·12 = 3120 mm², y1 = 6 mm
two legs: A2 = 2·12·78 = 1872 mm², y2 = 12 + 78/2 = 51 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.
Hogging: the top is in tension, the bottom in compression.
top edge: M = 60·2.945 × 10⁷/52.58 = 33.6 kN·m
bottom edge: M = 150·2.945 × 10⁷/187.4 = 23.57 kN·m
Governing value
Mallow = min = 23.57 kN·m (bottom edge)
Answer
Mallow = 23.57 kN·m
13.Effective stress in soil
Answer: σ′ = 136.8 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) = 9.81·7 = 68.67 kPa
Effective stress
σ′ = σ − u = 205.5 − 68.67 = 136.8 kPa
Answer
σ′ = 136.8 kPa
14.Effective stress in soil
Answer: σ′ = 88.14 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·3 + γsat,clay·3
σ = 16.5·2 + 19.5·3 + 18.5·3 = 147 kPa
Pore water pressure
Water pressure grows with depth below the water table.
u = γw·(z − zw) = 9.81·6 = 58.86 kPa
Effective stress
σ′ = σ − u = 147 − 58.86 = 88.14 kPa
Answer
σ′ = 88.14 kPa
15.Consolidation settlement
Answer: S = 51.87 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 + 80 = 130 kPa ≤ 150 kPa
Settlement
The clay stays on its recompression line.
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.04·5/(1 + 0.6)·log₁₀(130/50) = 51.87 mm
Answer
S = 51.87 mm
16.Consolidation settlement
Answer: t = 11.43 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 = 5.5 m
Time
t = Tv·Hdr²/cv = 0.567·5.5²/1.5 = 11.43 years
Answer
t = 11.43 years
17.Hydrostatic force
Answer: F = 82.77 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 + 2.5/2 = 2.25 m
A = H·b = 2.5·1.5 = 3.75 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·2.25·3.75 = 82.77 kN
Answer
F = 82.77 kN
18.Hydrostatic force
Answer: F = 12.36 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 = 0.5 + 1/2 = 1 m
A = H·b = 1·1 = 1 m²
Resultant force
F = ρ·g·yc·A = 1260·9.81·1·1 = 12.36 kN
Answer
F = 12.36 kN
19.Pipe friction & head loss
Answer: hf = 2.714 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) = 2.2²/(2·9.81) = 0.2467 m
Darcy–Weisbach
hf = f·(L/D)·V²/(2g) = 0.022·(100/0.2)·2.2²/(2·9.81) = 2.714 m
Answer
hf = 2.714 m
20.Pipe friction & head loss
Answer: Q = 13.32 L/s
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.
Loss coefficients
f·L/D = 0.02·150/0.1 = 30
ΣK = 0.5 + 2·0.3 + 2 + 1.0 = 4.1
Energy equation
Both surfaces are open to the air and practically at rest, so all of Δz is lost in the pipe.
Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.
Geometry
A = b·y = 4·1.5 = 6 m²
P = b + 2y = 4 + 2·1.5 = 7 m
R = A/P = 0.8571 m
Velocity
V = (1/0.03)·0.85712/3·0.00051/2 = 0.6726 m/s
Flow rate
Q = A·V = 6·0.6726 = 4.035 m³/s
Answer
Q = 4.035 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.002154 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 = 1000·9.81·0.015·26 = 3.826 kW
Shaft power
Pshaft = Ph/η = 3.826/0.82 = 4.666 kW
Answer
Pshaft = 4.666 kW
24.Pumps & pump power
Answer: Pshaft = 1.506 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 €18 000 yourself; the rest is interest.
27.NPV & IRR
Answer: NPV = 9628 €
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 = −30 000
CF1/(1 + 0.08)1 = 12 000/1.08 = 11 111.11
CF2/(1 + 0.08)2 = 12 000/1.166 = 10 288.07
CF3/(1 + 0.08)3 = 10 000/1.26 = 7 938.32
CF4/(1 + 0.08)4 = 14 000/1.36 = 10 290.42
Add them up
NPV = €9 627.92
Answer
NPV = €9 627.92
NPV is positive, so the project earns more than the required return.
28.NPV & IRR
Answer: MIRR = 15.47 %
Modified IRR: compound every inflow forward to the end of the project at the reinvestment rate (usually the cost of capital) to get the terminal value TV. MIRR is the rate that turns the initial investment into TV: MIRR = (TV/C₀)^(1/n) − 1.
Terminal value of the inflows
11 000·1.082 = 12 830.40
14 500·1.081 = 15 660.00
10 000·1.080 = 10 000.00
TV = 38 490.40
MIRR
MIRR = (38 490.40/25 000)1/3 − 1 = 15.47%
Answer
MIRR = 15.47%
29.Normal distribution
Answer: P = 0.5628
Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.
z-scores
z₁ = (96.25 − 100)/15 = −0.25
z₂ = (127 − 100)/15 = 1.8
Area between
P = Φ(1.8) − Φ(−0.25) = 0.9641 − 0.4013 = 0.5628
Answer
P = 0.5628
30.Normal distribution
Answer: x = 58.26 points
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.