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 1 mP2 = 50 kN at 2 m
RA = kN
2.Beam support reactionsHard
A compound beam is fixed to the wall at A, has an internal hinge at C (2 m from A) and rests on a roller at D (6 m from A). It carries a point load P at 4 m from A, a uniformly distributed load w on the whole part CD and a point load Q at 1.5 m from A. Find the magnitude of the reaction moment MA at the wall.
AC = 2 mAD = 6 mP = 25 kN at 4 mw = 8 kN/m from 2 to 6 mQ = 60 kN at 1.5 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 = 4 mheight = 3 mB is 1 m from Avertical load = 20 kN
FAB = kN
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.
B: 25 kN ↓G: 20 kN ↓H: 10 kN ↓H: 15 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
5.Shear force & bending momentMedium
The beam rests on a pin at A and a roller at B and overhangs B by 2 m to the free end C. It carries a point load P1 between the supports and a point load P2 at C. Find the bending moment MB at support B. Use sagging moments positive and upward shear on the left face positive.
L = 10 mP1 = 80 kN at 4 mP2 = 10 kN at 10 msupports at x = 0 and x = 8 m
MB = kN·m
6.Shear force & bending momentHard
Find the bending moment Mx at the section x = 2.5 m from support A. Use sagging moments positive and upward shear on the left face positive.
L = 5 mP = 45 kN at 2.5 mw = 3 kN/m from 0 to 5 mx = 2.5 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 = 6 mE = 70 GPa (aluminium)I = 84 × 10⁶ mm⁴
δmax = 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 = 29 kNw = 4 kN/mL = 5 mE = 200 GPa (steel)I = 8.5 × 10⁶ mm⁴
δmax = mm
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)d = 25 mm
Pcr = kN
10.Column bucklingHard
A column of length L made of aluminium is pinned at both ends. Find its slenderness and the critical buckling stress σcr from Euler’s formula.
L = 2.5 mE = 70 GPa (aluminium)d = 40 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 = 140 mmtf = 15 mmtw = 20 mmhw = 140 mm
Ix = × 10⁶ mm⁴
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 25 kN·m. Find the size of the bending stress σtop at the top edge.
A 4.5 m thick overconsolidated clay layer has Cc = 0.2, Cr = 0.05 and e₀ = 0.65. At its mid-depth the effective vertical stress is 95 kPa and the preconsolidation pressure is 155 kPa. A new building adds 30 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.
A clay layer 5 m thick has a coefficient of consolidation cv = 2 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 60% average consolidation the time factor is Tv = 0.287. How many years t does the layer take to reach 60% consolidation?
A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.
A vertical rectangular gate 1.5 m wide sits in the wall of a tank of seawater, with its top edge 1.5 m below the surface. Find the resultant hydrostatic force F on the gate.
Water flows at 60 L/s through a pipe 100 m long with an inside diameter of 250 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.
A pipe 300 m long with an inside diameter of 300 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 = 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 concrete storm sewer with an inside diameter of 300 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.0005. Find the flow rate Q in m³/s.
D = 300 mmn = 0.013S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
A rectangular unfinished concrete channel 2.5 m wide must carry 11 m³/s in uniform flow at a depth of 1.5 m. Manning n = 0.014. Find the required bed slope S (in m/m).
Q = 11 m³/sb = 2.5 my = 1.5 mn = 0.014
S = m/m
23.Pumps & pump powerMedium
A pump with an efficiency of 60% delivers 50 L/s of water (ρ = 1000 kg/m³) against a head of 44 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.
Q = 50 L/sH = 44 mη = 60%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
A pump moves 60 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 10 m higher. The pipe is 100 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 4 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.
You need €5 000 in 4 years. An account pays 3% per year, compounded monthly. How much must you deposit today? Find the present value PV.
FV = €5 0003% / 12n = 4
PV = €
26.Time value of moneyHard
You want €30 000 in 16 years. You save the same amount at the end of every month in an account paying 4.8% per year, compounded monthly. Find the monthly deposit A.
FV = €30 0004.8% / 12N = 192
A = €
27.NPV & IRRMedium
An investment of €75 000 gives these cash flows at the end of years 1 to 3: €27 000, €32 000, €26 000. The cost of capital is 12%. Find the net present value NPV.
A project costs €40 000 and returns €26 500, €22 000 at the end of years 1 to 2. Find its internal rate of return IRR in percent.
CF0 = −40 000CF1 = 26 500CF2 = 22 000
IRR = %
29.Normal distributionMedium
The exam scores are normally distributed with mean 65 points and standard deviation 10 points. What fraction lies between 57.5 and 77.5 points? Give P as a decimal.
μ = 65σ = 10x1 = 57.5x2 = 77.5
P =
30.Normal distributionHard
The mass X of a product from line 1 and Y from line 2 are independent and normal: X has mean 500 g and standard deviation 8 g, Y has mean 490 g and standard deviation 6 g. Find the probability P that X is greater than Y. Round z to two decimals.
μX = 500 g, σX = 8 gμY = 490 g, σY = 6 g
P =
3Solutions
1.Beam support reactions
Answer: RA = 66.25 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 = 55·1 + 50·2
RB = 155/4 = 38.75 kN
ΣFy = 0: RA = 105 − 38.75 = 66.25 kN
Answer
RA = 66.25 kN
2.Beam support reactions
Answer: MA = 147 kN·m
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. An internal hinge cannot carry a bending moment, which gives one extra equation: the moment about the hinge of the forces on either side is zero.
Part CD
The hinge has no moment, so moments about C on CD alone must balance.
W = 8·4 = 32 kN at 2 m from C
ΣMC = 0: RD·4 = 25·2 + 32·2
RD = 28.5 kN
VC = 57 − 28.5 = 28.5 kN
Part AC
The hinge force VC acts downward on AC (equal and opposite to its action on CD).
RA = 60 + 28.5 = 88.5 kN
MA = 60·1.5 + 28.5·2 = 147 kN·m
Answer
MA = 147 kN·m
3.Truss: method of joints
Answer: FAB = −15.81 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·4 = 20·1 → Cy = 5 kN
ΣFy = 0: Ay = 20 − 5 = 15 kN
Joint A
Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.
sin α = 3/3.162 = 0.9487
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −15/0.9487 = −15.81 kN
Answer
FAB = −15.81 kN (compression)
4.Truss: method of joints
Answer: member DH
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.
Support reactions
Equilibrium of the whole beam. The overhang load also acts about A.
ΣMA = 0: RB·8 = 80·4 + 10·10
RB = 420/8 = 52.5 kN
ΣFy = 0: RA = 90 − 52.5 = 37.5 kN
Cut at B and keep the overhang
Only P2 acts on the overhang, with lever arm a. It bends the beam upward over the support (hogging).
MB = −P2·a = −10·2 = −20 kN·m
Answer
MB = −20 kN·m
6.Shear force & bending moment
Answer: Mx = 65.63 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 = 3·5 = 15 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 45·2.5 + 3·5·2.5
RB = 150/5 = 30 kN
ΣFy = 0: RA = 60 − 30 = 30 kN
Cut at x = 2.5 m and keep the left part
Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.
M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 30·2.5 − 3·2.5·1.25 = 65.63 kN·m
Answer
Mx = 65.63 kN·m
7.Beam deflection
Answer: δmax = 17.22 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 = 6000 mm
EI = 5.88 × 10¹² N·mm²
Deflection
δmax = 5wL⁴/(384EI) = 5·6·6000⁴/(384·5.88 × 10¹²) = 17.22 mm
Answer
δmax = 17.22 mm
8.Beam deflection
Answer: δmax = 63.57 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 = 29000 N, w = 4 N/mm, L = 5000 mm, EI = 1.7 × 10¹² N·mm²
Each load on its own
δP = PL³/(48EI) = 29000·5000³/(48·1.7 × 10¹²) = 44.42 mm
δw = 5wL⁴/(384EI) = 5·4·5000⁴/(384·1.7 × 10¹²) = 19.15 mm
Add them
δmax = 44.42 + 19.15 = 63.57 mm
Answer
δmax = 63.57 mm
9.Column buckling
Answer: Pcr = 16.82 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·40⁴/64 = 125664 mm⁴
Radius of gyration and slenderness
A = 1257 mm²
r = √(I/A) = √(125664/1257) = 10 mm
KL = 1·2500 = 2500 mm
KL/r = 2500/10 = 250
Critical stress
σcr = π²E/(KL/r)² = π²·70000/250² = 11.05 MPa
Answer
σcr = 11.05 MPa
11.Centroid & second moment of area
Answer: Ix = 11.82 × 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 = 140·15 = 2100 mm², yf = 140 + 15/2 = 147.5 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 two rectangles
Measure every y from the bottom edge.
flange: Af = 100·25 = 2500 mm², yf = 120 + 25/2 = 132.5 mm
Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).
Pore water pressure
Water pressure grows with depth below the water table.
u = γw·(z − zw) = 9.81·6 = 58.86 kPa
Answer
u = 58.86 kPa
14.Effective stress in soil
Answer: σ′ = 81.76 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·3 + γsat,sand·1 + γsat,clay·3
σ = 16·3 + 20.5·1 + 17.5·3 = 121 kPa
Pore water pressure
Water pressure grows with depth below the water table.
u = γw·(z − zw) = 9.81·4 = 39.24 kPa
Effective stress
σ′ = σ − u = 121 − 39.24 = 81.76 kPa
Answer
σ′ = 81.76 kPa
15.Consolidation settlement
Answer: S = 16.25 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 + 30 = 125 kPa ≤ 155 kPa
Settlement
The clay stays on its recompression line.
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·4.5/(1 + 0.65)·log₁₀(125/95) = 16.25 mm
Answer
S = 16.25 mm
16.Consolidation settlement
Answer: t = 0.8969 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 = 5/2 = 2.5 m
Time
t = Tv·Hdr²/cv = 0.287·2.5²/2 = 0.8969 years
Answer
t = 0.8969 years
17.Hydrostatic force
Answer: F = 36.79 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 + 1.5/2 = 1.25 m
A = H·b = 1.5·2 = 3 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·1.25·3 = 36.79 kN
Answer
F = 36.79 kN
18.Hydrostatic force
Answer: F = 75.41 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 = 1.5 + 2/2 = 2.5 m
A = H·b = 2·1.5 = 3 m²
Resultant force
F = ρ·g·yc·A = 1025·9.81·2.5·3 = 75.41 kN
Answer
F = 75.41 kN
19.Pipe friction & head loss
Answer: hf = 0.9138 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.
Mean velocity
A = π·0.25²/4 = 0.04909 m²
V = Q/A = 0.06/0.04909 = 1.222 m/s
Velocity head
V²/(2g) = 1.222²/(2·9.81) = 0.07615 m
Darcy–Weisbach
hf = f·(L/D)·V²/(2g) = 0.03·(100/0.25)·1.222²/(2·9.81) = 0.9138 m
Answer
hf = 0.9138 m
20.Pipe friction & head loss
Answer: H = 1.743 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 = 0.08/0.07069 = 1.132 m/s
V²/(2g) = 0.06529 m
Loss coefficients
f·L/D = 0.022·300/0.3 = 22
ΣK = 0.5 + 4·0.3 + 2 = 3.7
Energy equation
The outlet jet still carries its velocity head; it is not a loss but it has to be supplied.
H = (1 + 22 + 3.7)·0.06529 = 1.743 m
Answer
H = 1.743 m
21.Open-channel flow (Manning)
Answer: Q = 0.02162 m³/s
Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.
Geometry
A = 0.07069 m², R = D/4 = 0.075 m
Velocity
V = (1/0.013)·0.0752/3·0.00051/2 = 0.3059 m/s
Flow rate
Q = A·V = 0.07069·0.3059 = 0.02162 m³/s
Answer
Q = 0.02162 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.00281 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 = 1000·9.81·0.05·44 = 21.58 kW
Shaft power
Pshaft = Ph/η = 21.58/0.6 = 35.97 kW
Answer
Pshaft = 35.97 kW
24.Pumps & pump power
Answer: H = 12.42 m
Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.
Both surfaces are open and practically at rest, so pressure and velocity terms drop out.
H = Δz + hL = 10 + 2.417 = 12.42 m
Answer
H = 12.42 m
25.Time value of money
Answer: PV = 4435 €
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 = 0.03/12 = 0.0025
N = 12·4 = 48
Present value
PV = FV/(1 + i)N = 5 000/1.127 = €4 435.27
Answer
PV = €4 435.27
26.Time value of money
Answer: A = 104.2 €
Time value of money: money today is worth more than the same amount later, because it can earn interest. With interest rate i per period, an amount grows as FV = PV·(1 + i)n. A series of equal payments (an annuity) is valued by adding up each payment, which gives the annuity formulas.
Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.
Present value of each cash flow
CF0 = −75 000
CF1/(1 + 0.12)1 = 27 000/1.12 = 24 107.14
CF2/(1 + 0.12)2 = 32 000/1.254 = 25 510.20
CF3/(1 + 0.12)3 = 26 000/1.405 = 18 506.29
Add them up
NPV = €−6 876.37
Answer
NPV = €−6 876.37
NPV is negative, so the project earns less than the required return.
28.NPV & IRR
Answer: IRR = 14.35 %
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(10%) = 2 272.73
NPV(15%) = −321.36
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 = (57.5 − 65)/10 = −0.75
z₂ = (77.5 − 65)/10 = 1.25
Area between
P = Φ(1.25) − Φ(−0.75) = 0.8944 − 0.2266 = 0.6677
Answer
P = 0.6677
30.Normal distribution
Answer: P = 0.8413
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 = 500 − 490 = 10 g, σ = 10 g
Standardise
z = (0 − 10)/10 = −1
Probability
P = 1 − Φ(−1) = 0.8413
Answer
P = 0.8413
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