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 = 6 mP1 = 15 kN at 2 mP2 = 50 kN at 2.5 m
RB = kN
2.Beam support reactionsHard
The cantilever beam is fixed to the wall at A. It carries a linearly varying load that is zero at the wall and rises to 8 kN/m at the free end B, plus a point load P at 3 m from the wall. Find the magnitude of the reaction moment MA at the wall.
L = 5 mw0 = 8 kN/mP = 60 kN at 3 m
MA = kN·m
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 = 4 mB is 4 m from Avertical load = 50 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 = 6 mheight = 4 mB is 2 m from Avertical load = 25 kNhorizontal load = 15 kN →
FBC = 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 @ 2 m10 kN @ 10 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 = 3.5 m from support A. Use sagging moments positive and upward shear on the left face positive.
L = 6 mP = 10 kN at 3.5 mw = 12 kN/m from 0 to 6 mx = 3.5 m
Mx = 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 = 6 kN/mL = 3 mE = 200 GPa (steel)I = 8.5 × 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 = 5 kN/mL = 6 mE = 11 GPa (timber)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
A column of length L made of aluminium is fixed at the base and free at the top. Using Euler’s formula, find its critical buckling load Pcr.
L = 1 mE = 70 GPa (aluminium)d = 80 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 = 20 mm
σcr = MPa
11.Centroid & second moment of areaMedium
Find the second moment of area Ix of the T-section about the horizontal axis x through its centroid.
bf = 280 mmtf = 20 mmtw = 14 mmhw = 300 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
A 120 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 105 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.
b = 120 mmh = 150 mmcut-out: 60 × 40 mmhole centre: y = 105 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
For the soil profile shown, find the pore water pressure u at point X.
A 2.5 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.03 and e₀ = 1. At its mid-depth the effective vertical stress is 50 kPa and the preconsolidation pressure is 160 kPa. A new building adds 35 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.
A clay layer 6.5 m thick has a coefficient of consolidation cv = 1.5 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 90% average consolidation the time factor is Tv = 0.848. How many years t does the layer take to reach 90% consolidation?
A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 2.5 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 water, with its top edge 2 m below the surface. Find the depth ycp of the centre of pressure below the surface.
d = 2 mH = 3 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
Water (ρ = 1000 kg/m³) flows at 1.7 m/s through a horizontal pipe, 1000 m long, with an inside diameter of 100 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.
Two open reservoirs are joined by a pipe 300 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.015. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each), a valve (K = 5) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². What difference in water level Δz between the reservoirs gives a flow rate of 60 L/s?
A trapezoidal unfinished concrete channel has a bottom width of 6 m and side slopes of 1:1 (horizontal:vertical). Water flows uniformly 2.2 m deep. Manning n = 0.014 and the bed slope is S = 0.004. Find the flow rate Q in m³/s.
b = 6 my = 2.2 mz = 1n = 0.014S = 0.004
Q = m³/s
22.Open-channel flow (Manning)Hard
A trapezoidal clean earth channel with a bottom width of 4 m and side slopes of 2:1 (horizontal:vertical) must carry 25 m³/s in uniform flow at a depth of 2.3 m. Manning n = 0.022. Find the required bed slope S (in m/m).
Q = 25 m³/sb = 4 my = 2.3 mz = 2n = 0.022
S = m/m
23.Pumps & pump powerMedium
In a test, a pump delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 18 m while its shaft takes 13.2 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.
Q = 60 L/sH = 18 mPshaft = 13.2 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
A pump moves 80 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 200 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 = 3 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 80%. Find the shaft power Pshaft in kW.
You need €5 000 in 5 years. An account pays 4.8% per year, compounded quarterly. How much must you deposit today? Find the present value PV.
FV = €5 0004.8% / 4n = 5
PV = €
26.Time value of moneyHard
You save €150 at the end of every month for 22 years. The account pays 3.6% per year, compounded monthly. How much have you saved at the end? Find FV.
A = €1503.6% / 12N = 264
FV = €
27.NPV & IRRMedium
A project costs €250 000 today. It generates €14 000 at the end of the first year, and the cash flow then grows by 2% per year forever. The cost of capital is 9%. Find the net present value NPV.
C0 = €250 000CF1 = €14 000g = 2%r = 9%
NPV = €
28.NPV & IRRHard
A project costs €40 000 and returns €24 000, €27 500, €24 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.
CF0 = −40 000CF1 = 24 000CF2 = 27 500CF3 = 24 000
IRR = %
29.Normal distributionMedium
The delivery times are normally distributed with mean 32 min and standard deviation 6 min. What fraction lies between 30.2 and 39.5 min? Give P as a decimal.
μ = 32σ = 6x1 = 30.2x2 = 39.5
P =
30.Normal distributionHard
Runner A's lap time X and runner B's lap time Y are independent and normal: X has mean 52 s and standard deviation 4 s, Y has mean 48 s and standard deviation 3 s. Find the probability P that X is greater than Y. Round z to two decimals.
μX = 52 s, σX = 4 sμY = 48 s, σY = 3 s
P =
3Solutions
1.Beam support reactions
Answer: RB = 25.83 kN
Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Taking moments about one support removes that support’s reaction from the equation.
Free-body diagram
Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.
Equilibrium
Moments about A, counter-clockwise positive. Then vertical force balance.
ΣMA = 0: RB·6 = 15·2 + 50·2.5
RB = 155/6 = 25.83 kN
ΣFy = 0: RA = 65 − 25.83 = 39.17 kN
Answer
RB = 25.83 kN
2.Beam support reactions
Answer: MA = 246.7 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 triangular load
W = ½·8·5 = 20 kN
x̄ = 2L/3 = 3.333 m
Moment about the wall
MA = W·x̄ + P·a = 20·3.333 + 60·3 = 246.7 kN·m
Answer
MA = 246.7 kN·m
3.Truss: method of joints
Answer: FAB = −14.14 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 = 50·4 → Cy = 40 kN
ΣFy = 0: Ay = 50 − 40 = 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 = 4/5.657 = 0.7071
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −10/0.7071 = −14.14 kN
Answer
FAB = −14.14 kN (compression)
4.Truss: method of joints
Answer: FBC = −25.93 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·6 = 25·2 + 15·4 → Cy = 18.33 kN
ΣFy = 0: Ay = 25 − 18.33 = 6.667 kN
ΣFx = 0: Ax = −15 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 = 4/5.657 = 0.7071, cos γ = 4/5.657 = 0.7071
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 = 18.33 kN, R2 = 11.67 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 = 36.67 kN·m, MC = 33.33, MD = 30, ME = 26.67, MF = 23.33, MG = 0
Answer
Mark B: MB = 36.67 kN·m
6.Shear force & bending moment
Answer: Mx = 67.08 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 = 12·6 = 72 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 10·3.5 + 12·6·3
RB = 251/6 = 41.83 kN
ΣFy = 0: RA = 82 − 41.83 = 40.17 kN
Cut at x = 3.5 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 = 40.17·3.5 − 12·3.5·1.75 = 67.08 kN·m
Answer
Mx = 67.08 kN·m
7.Beam deflection
Answer: δmax = 3.722 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.
w = 6 N/mm, L = 3000 mm
EI = 1.7 × 10¹² N·mm²
Deflection
δmax = 5wL⁴/(384EI) = 5·6·3000⁴/(384·1.7 × 10¹²) = 3.722 mm
Answer
δmax = 3.722 mm
8.Beam deflection
Answer: Ireq = 460.2 × 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 = 6000/360 = 16.67 mm
Required second moment of area
I = 5wL⁴/(384·E·δallow) = 5·5·6000⁴/(384·11000·16.67) = 4.602 × 10⁸ mm⁴
Ireq = 460.2 × 10⁶ mm⁴
Answer
Ireq = 460.2 × 10⁶ mm⁴
9.Column buckling
Answer: Pcr = 347.3 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.
Smallest second moment of area
A round section has the same I about every axis.
I = πd⁴/64 = π·20⁴/64 = 7854 mm⁴
Radius of gyration and slenderness
A = 314.2 mm²
r = √(I/A) = √(7854/314.2) = 5 mm
KL = 0.7·1000 = 700 mm
KL/r = 700/5 = 140
Critical stress
σcr = π²E/(KL/r)² = π²·200000/140² = 100.7 MPa
Answer
σcr = 100.7 MPa
11.Centroid & second moment of area
Answer: Ix = 93.13 × 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 = 280·20 = 5600 mm², yf = 300 + 20/2 = 310 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 = (18000·75 − 2400·105)/(18000 − 2400) = 70.38 mm
Full plate about ȳ
120·150³/12 + 18000·4.615² = 34.13 × 10⁶ mm⁴
Hole about ȳ
60·40³/12 + 2400·34.62² = 3.196 × 10⁶ mm⁴
Subtract
Ix = 30.94 × 10⁶ mm⁴
Answer
Ix = 30.94 × 10⁶ mm⁴
13.Effective stress in soil
Answer: u = 9.81 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) = 9.81·1 = 9.81 kPa
Answer
u = 9.81 kPa
14.Effective stress in soil
Answer: u = 49.05 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) = 9.81·5 = 49.05 kPa
Answer
u = 49.05 kPa
15.Consolidation settlement
Answer: S = 8.642 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 + 35 = 85 kPa ≤ 160 kPa
Settlement
The clay stays on its recompression line.
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.03·2.5/(1 + 1)·log₁₀(85/50) = 8.642 mm
Answer
S = 8.642 mm
16.Consolidation settlement
Answer: t = 5.971 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 = 6.5/2 = 3.25 m
Time
t = Tv·Hdr²/cv = 0.848·3.25²/1.5 = 5.971 years
Answer
t = 5.971 years
17.Hydrostatic force
Answer: F = 58.86 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 + 1/2 = 3 m
A = H·b = 1·2 = 2 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·3·2 = 58.86 kN
Answer
F = 58.86 kN
18.Hydrostatic force
Answer: ycp = 3.714 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 = 2 + 3/2 = 3.5 m
A = H·b = 3·1 = 3 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·3.5·3 = 103 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) = 0.03·(1000/0.1)·1.7²/(2·9.81) = 44.19 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 = 0.06/0.03142 = 1.91 m/s
V²/(2g) = 0.1859 m
Loss coefficients
f·L/D = 0.015·300/0.2 = 22.5
ΣK = 0.5 + 2·0.3 + 5 + 1.0 = 7.1
Total head loss
hf = 22.5·0.1859 = 4.183 m
hm = 7.1·0.1859 = 1.32 m
Δz = hf + hm = 5.503 m
Answer
Δz = 5.503 m
21.Open-channel flow (Manning)
Answer: Q = 105.6 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 = (6 + 1·2.2)·2.2 = 18.04 m²
P = b + 2y·√(1 + z²) = 6 + 2·2.2·√(1 + 1²) = 12.22 m
R = A/P = 1.476 m
Velocity
V = (1/0.014)·1.4762/3·0.0041/2 = 5.856 m/s
Flow rate
Q = A·V = 18.04·5.856 = 105.6 m³/s
Answer
Q = 105.6 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.000501 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 = (4 + 2·2.3)·2.3 = 19.78 m²
P = b + 2y·√(1 + z²) = 4 + 2·2.3·√(1 + 2²) = 14.29 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 = 1000·9.81·0.06·18 = 10.59 kW
Efficiency
η = Ph/Pshaft = 10.59/13.2 = 80.26%
Answer
η = 80.26%
24.Pumps & pump power
Answer: Pshaft = 12.69 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 = 0.048/4 = 0.012
N = 4·5 = 20
Present value
PV = FV/(1 + i)N = 5 000/1.269 = €3 938.76
Answer
PV = €3 938.76
26.Time value of money
Answer: FV = 60260 €
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 €39 600 yourself; the rest is interest.
27.NPV & IRR
Answer: NPV = −50000 €
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.
Value of the cash flows
PV = 14 000/(0.09 − 0.02) = 200 000.00
NPV
NPV = 200 000.00 − 250 000 = −€50 000.00
Answer
NPV = −€50 000.00
NPV is negative, so the project earns less than the required return.
28.NPV & IRR
Answer: IRR = 39.84 %
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(35%) = 2 621.55
NPV(40%) = −80.17
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.
z-scores
z₁ = (30.2 − 32)/6 = −0.3
z₂ = (39.5 − 32)/6 = 1.25
Area between
P = Φ(1.25) − Φ(−0.3) = 0.8944 − 0.3821 = 0.5123
Answer
P = 0.5123
30.Normal distribution
Answer: P = 0.7881
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 = 52 − 48 = 4 s, σ = 5 s
Standardise
z = (0 − 4)/5 = −0.8
Probability
P = 1 − Φ(−0.8) = 0.7881
Answer
P = 0.7881
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