laminar below Re ≈ 2000, turbulent above Re ≈ 4000
Mean velocity
V = Q/A, A = π·D²/4
Darcy–Weisbach
hf = f·(L/D)·V²/(2g)
Minor losses
hm = ΣK·V²/(2g)
Typical K values
entrance 0.5, exit 1.0, 90° bend ≈ 0.3
Pressure drop
Δp = ρ·g·hf
Two open reservoirs
Δz = (f·L/D + ΣK)·V²/(2g)
Free outlet
H = (1 + f·L/D + ΣK)·V²/(2g)
Open-channel flow (Manning)
Manning equation
V = (1/n)·R2/3·S1/2
Flow rate
Q = A·V
Hydraulic radius
R = A/P (P = wetted perimeter, free surface excluded)
Rectangle
A = b·y, P = b + 2y
Trapezoid (side slope z:1)
A = (b + z·y)·y, P = b + 2y·√(1 + z²)
Circular pipe, full or half full
R = D/4
Required slope
S = (n·Q/(A·R2/3))²
Pumps & pump power
Hydraulic power
Ph = ρ·g·Q·H = Q·Δp
Shaft power
Pshaft = Ph/ηpump
Electrical power
Pel = Pshaft/ηmotor
Pump head
H = Δz + Δp/(ρ·g) + hL
System losses
hL = (f·L/D + ΣK)·V²/(2g)
Time value of money
Future value
FV = PV·(1 + i)n
Present value
PV = FV/(1 + i)n
Several periods per year
i = r/m, N = m·n
Annuity, present value
PV = PMT·[1 − (1 + i)−n]/i
Annuity, future value
FV = PMT·[(1 + i)n − 1]/i
Method
Draw a timeline with every cash flow and its timing.
Match the rate to the period: a monthly rate for monthly payments.
Use FV = PV·(1 + i)ⁿ for single amounts and the annuity formulas for equal payments.
Check the sign and the order of magnitude of the answer.
NPV & IRR
Net present value
NPV = −C0 + Σ CFt/(1 + r)t
Equal cash flows
NPV = −C0 + CF·[1 − (1 + r)−n]/r
Internal rate of return
the r at which NPV = 0
Decision
accept when NPV > 0 (or IRR > required return)
Method
List all cash flows with their year; the investment at year 0 is negative.
Discount each cash flow: CFt/(1 + r)t.
Add them up to get the NPV. Positive means the project earns more than r.
For the IRR, find the rate that makes NPV zero by trial or interpolation.
Normal distribution
z-score
z = (x − μ)/σ
Below x
P(X < x) = Φ(z)
Above x
P(X > x) = 1 − Φ(z)
Between
Φ(z2) − Φ(z1)
Percentile
x = μ + z·σ
Method
Convert the value to a z-score: z = (x − μ)/σ.
Look up Φ(z), the area to the left of z.
For the area to the right use 1 − Φ(z); for an interval subtract the two left areas.
For a percentile, work backwards: find z for the area, then x = μ + z·σ.
2Practice problems
1.Beam support reactionsMedium
The simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RB.
L = 4 mP1 = 55 kN at 1 mP2 = 55 kN at 2 m
RB = kN
2.Beam support reactionsHard
A compound beam is fixed to the wall at A, has an internal hinge at C (4 m from A) and rests on a roller at D (8 m from A). It carries a point load P at 6 m from A, a uniformly distributed load w on the whole part CD and a point load Q at 2 m from A. Find the magnitude of the reaction moment MA at the wall.
AC = 4 mAD = 8 mP = 75 kN at 6 mw = 8 kN/m from 4 to 8 mQ = 65 kN at 2 m
MA = kN·m
3.Truss: method of jointsMedium
Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.
B: 10 kN ↓D: 40 kN ↓F: 20 kN ↓H: 10 kN ↓
1member AB
2member BC
3member CD
4member DE
5member FG
6member GH
7member AF
8member HE
9member BF
10member CG
11member DH
12member FC
13member HC
4.Truss: method of jointsHard
Use the method of joints to find the force FAB in member AB. Give tension as positive and compression as negative.
span = 8 mheight = 3 mB is 3 m from Avertical load = 50 kNhorizontal load = 5 kN ←
FAB = 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.
45 kN @ 2 m30 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 = 4 m from support A. Use sagging moments positive and upward shear on the left face positive.
L = 8 mP = 25 kN at 4 mw = 3 kN/m from 0 to 8 mx = 4 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 = 10 kN/mL = 6 mE = 200 GPa (steel)I = 57 × 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 = 16 kNw = 20 kN/mL = 3 mE = 11 GPa (timber)I = 120 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
A column of length L made of steel is fixed at the base and pinned at the top. Using Euler’s formula, find its critical buckling load Pcr.
L = 4 mE = 200 GPa (steel)b × h = 30 × 60 mm
Pcr = kN
10.Column bucklingHard
A solid round column of length L made of steel is fixed at both ends. It must carry 115 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.
P = 115 kNn = 3L = 6 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
Find the second moment of area Ix of the T-section about the horizontal axis x through its centroid.
bf = 140 mmtf = 20 mmtw = 20 mmhw = 160 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
A welded I-section has a top flange 200 × 18 mm, a web 380 mm high and 10 mm thick, and a bottom flange 280 × 20 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.
top flange: 200 × 18 mmweb: 10 × 380 mmbottom flange: 280 × 20 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 m thick overconsolidated clay layer has Cc = 0.4, Cr = 0.04 and e₀ = 0.6. At its mid-depth the effective vertical stress is 55 kPa and the preconsolidation pressure is 85 kPa. A new building adds 160 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.
A clay layer 3 m thick has a coefficient of consolidation cv = 5 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. 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 3 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.
d = 2 mH = 2 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
A vertical rectangular gate 3 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 (ρ = 1000 kg/m³) flows at 1 m/s through a horizontal pipe, 300 m long, with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.02 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 200 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), 3 bends (K = 0.3 each) and a valve (K = 10). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 75 L/s?
A trapezoidal unfinished concrete channel has a bottom width of 3 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 2 m deep. Manning n = 0.014 and the bed slope is S = 0.005. Find the flow rate Q in m³/s.
b = 3 my = 2 mz = 3n = 0.014S = 0.005
Q = m³/s
22.Open-channel flow (Manning)Hard
A trapezoidal clean earth channel with a bottom width of 4.5 m and side slopes of 2:1 (horizontal:vertical) must carry 21 m³/s in uniform flow at a depth of 1.2 m. Manning n = 0.022. Find the required bed slope S (in m/m).
Q = 21 m³/sb = 4.5 my = 1.2 mz = 2n = 0.022
S = m/m
23.Pumps & pump powerMedium
In a test, a pump delivers 15 L/s of water (ρ = 1000 kg/m³) against a head of 30 m while its shaft takes 5.2 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.
Q = 15 L/sH = 30 mPshaft = 5.2 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
A pump moves 120 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 13 m higher. The pipe is 300 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 78%. Find the shaft power Pshaft in kW.
You invest €20 000 at a nominal rate of 4% per year, compounded quarterly. Find the value FV of the investment after 3 years.
PV = €20 0004% / 4n = 3
FV = €
26.Time value of moneyHard
A loan of €20 000 is repaid with equal monthly payments over 4 years at 5.4% per year, compounded monthly. How much interest I is paid in total over the life of the loan?
P = €20 0005.4% / 12N = 48
I = €
27.NPV & IRRMedium
An investment of €45 000 gives these cash flows at the end of years 1 to 4: €16 000, €14 000, €18 000, €10 000. The cost of capital is 10%. Find the net present value NPV.
A project costs €50 000 and returns €30 000, €36 500, €27 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.
CF0 = −50 000CF1 = 30 000CF2 = 36 500CF3 = 27 500
IRR = %
29.Normal distributionMedium
Drag z so that the shaded area between −z and z under the standard normal curve is 0.7580. Find z to two decimals.
A = 0.7580
z =
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 top 15% is to the right of it. Find the cut-off x.
μ = 65 pointsσ = 10 points15%
x = points
3Solutions
1.Beam support reactions
Answer: RB = 41.25 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 + 55·2
RB = 165/4 = 41.25 kN
ΣFy = 0: RA = 110 − 41.25 = 68.75 kN
Answer
RB = 41.25 kN
2.Beam support reactions
Answer: MA = 344 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 = 75·2 + 32·2
RD = 53.5 kN
VC = 107 − 53.5 = 53.5 kN
Part AC
The hinge force VC acts downward on AC (equal and opposite to its action on CD).
RA = 65 + 53.5 = 118.5 kN
MA = 65·2 + 53.5·4 = 344 kN·m
Answer
MA = 344 kN·m
3.Truss: method of joints
Answer: member CG
Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.
Joint G
FG and GH lie on one straight line and the joint carries no load. Balancing forces across that line leaves only CG.
ΣF⊥ = 0 → FCG = 0
Check with the method of joints
Solving all joints gives these member forces (T = tension, C = compression).
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 = 50·3 − 5·3 → Cy = 16.88 kN
ΣFy = 0: Ay = 50 − 16.88 = 33.13 kN
ΣFx = 0: Ax = 5 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 = −33.13/0.7071 = −46.85 kN
Answer
FAB = −46.85 kN (compression)
5.Shear force & bending moment
Answer: D (x = 6 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 = 52.5 kN, R2 = 22.5 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 = 105, MC = 120, MD = 135 kN·m, ME = 90, MF = 45, MG = 0
Answer
Mark D: MD = 135 kN·m
6.Shear force & bending moment
Answer: Mx = 74 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 = 3·8 = 24 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 25·4 + 3·8·4
RB = 196/8 = 24.5 kN
ΣFy = 0: RA = 49 − 24.5 = 24.5 kN
Cut at x = 4 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 = 24.5·4 − 3·4·2 = 74 kN·m
Answer
Mx = 74 kN·m
7.Beam deflection
Answer: δmax = 14.8 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 = 10 N/mm, L = 6000 mm
EI = 1.14 × 10¹³ N·mm²
Deflection
δmax = 5wL⁴/(384EI) = 5·10·6000⁴/(384·1.14 × 10¹³) = 14.8 mm
Answer
δmax = 14.8 mm
8.Beam deflection
Answer: δmax = 22.8 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 = 16000 N, w = 20 N/mm, L = 3000 mm, EI = 1.32 × 10¹² N·mm²
Each load on its own
δP = PL³/(48EI) = 16000·3000³/(48·1.32 × 10¹²) = 6.818 mm
δw = 5wL⁴/(384EI) = 5·20·3000⁴/(384·1.32 × 10¹²) = 15.98 mm
Add them
δmax = 6.818 + 15.98 = 22.8 mm
Answer
δmax = 22.8 mm
9.Column buckling
Answer: Pcr = 33.99 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.
Required critical load
Pcr = n·P = 3·115000 = 345000 N
KL = 0.5·6000 = 3000 mm
Solve for the diameter
d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·345000·3000²/(π³·200000))^(1/4) = 75.24 mm
Answer
d = 75.24 mm
Check: the slenderness KL/r is 159.5, so the column is slender and Euler applies.
11.Centroid & second moment of area
Answer: Ix = 19.02 × 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 = 140·20 = 2800 mm², yf = 160 + 20/2 = 170 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 three rectangles
Measure every y from the bottom edge.
top flange: A = 3600 mm², y = 409 mm
web: A = 3800 mm², y = 210 mm
bottom flange: A = 5600 mm², y = 10 mm
Centroid
ȳ = (3600·409 + 3800·210 + 5600·10)/13000 = 179 mm
Parallel-axis theorem
top flange: 200·18³/12 + 3600·230² = 1.906 × 10⁸ mm⁴
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
14.Effective stress in soil
Answer: σ = 135.5 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·1 + γsat,sand·3 + γsat,clay·3.5
σ = 15.5·1 + 19·3 + 18·3.5 = 135.5 kPa
Answer
σ = 135.5 kPa
15.Consolidation settlement
Answer: S = 211 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 = 55 + 160 = 215 kPa > 85 kPa
Settlement
Recompression up to σ′p, virgin compression beyond it.
S = 0.04·2/(1 + 0.6)·log₁₀(85/55) + 0.4·2/(1 + 0.6)·log₁₀(215/85)
S = 9.453 + 201.5 = 211 mm
Answer
S = 211 mm
16.Consolidation settlement
Answer: t = 0.08865 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 = 3/2 = 1.5 m
Time
t = Tv·Hdr²/cv = 0.197·1.5²/5 = 0.08865 years
Answer
t = 0.08865 years
17.Hydrostatic force
Answer: F = 176.6 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 + 2/2 = 3 m
A = H·b = 2·3 = 6 m²
Resultant force
F = ρ·g·yc·A = 1000·9.81·3·6 = 176.6 kN
Answer
F = 176.6 kN
18.Hydrostatic force
Answer: F = 101.8 kN
Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.
Centroid depth and area
yc = d + H/2 = 1.5 + 1.5/2 = 2.25 m
A = H·b = 1.5·3 = 4.5 m²
Resultant force
F = ρ·g·yc·A = 1025·9.81·2.25·4.5 = 101.8 kN
Answer
F = 101.8 kN
19.Pipe friction & head loss
Answer: Δp = 10 kPa
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) = 0.02·(300/0.3)·1²/(2·9.81) = 1.019 m
Pressure drop
The pipe is horizontal and the velocity does not change, so the energy equation reduces to Δp = ρ·g·hf.
Δp = ρ·g·hf = 1000·9.81·1.019 = 10000 Pa = 10 kPa
Answer
Δp = 10 kPa
20.Pipe friction & head loss
Answer: H = 7.959 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 = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m
Loss coefficients
f·L/D = 0.015·200/0.2 = 15
ΣK = 0.5 + 3·0.3 + 10 = 11.4
Energy equation
The outlet jet still carries its velocity head; it is not a loss but it has to be supplied.
H = (1 + 15 + 11.4)·0.2905 = 7.959 m
Answer
H = 7.959 m
21.Open-channel flow (Manning)
Answer: Q = 99.8 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 = (3 + 3·2)·2 = 18 m²
P = b + 2y·√(1 + z²) = 3 + 2·2·√(1 + 3²) = 15.65 m
R = A/P = 1.15 m
Velocity
V = (1/0.014)·1.152/3·0.0051/2 = 5.545 m/s
Flow rate
Q = A·V = 18·5.545 = 99.8 m³/s
Answer
Q = 99.8 m³/s
22.Open-channel flow (Manning)
Answer: S = 0.003933 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 = (4.5 + 2·1.2)·1.2 = 8.28 m²
P = b + 2y·√(1 + z²) = 4.5 + 2·1.2·√(1 + 2²) = 9.867 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 = 1000·9.81·0.015·30 = 4.415 kW
Efficiency
η = Ph/Pshaft = 4.415/5.2 = 84.89%
Answer
η = 84.89%
24.Pumps & pump power
Answer: Pshaft = 37.09 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.
Monthly payment
i = 0.0045, N = 48
A = 20 000·0.0045/(1 − (1 + 0.0045)−48) = €464.22
Total interest
I = N·A − P = 48·464.2 − 20 000 = €2 282.49
Answer
I = €2 282.49
27.NPV & IRR
Answer: NPV = 1470 €
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 = −45 000
CF1/(1 + 0.1)1 = 16 000/1.1 = 14 545.45
CF2/(1 + 0.1)2 = 14 000/1.21 = 11 570.25
CF3/(1 + 0.1)3 = 18 000/1.331 = 13 523.67
CF4/(1 + 0.1)4 = 10 000/1.464 = 6 830.13
Add them up
NPV = €1 469.50
Answer
NPV = €1 469.50
NPV is positive, so the project earns more than the required return.
28.NPV & IRR
Answer: IRR = 40.12 %
Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.
Bracket the IRR
NPV falls as the rate rises, so the IRR lies between a rate with positive NPV and one with negative NPV.
NPV(40%) = 72.89
NPV(45%) = −2 929.60
Narrow down
Linear interpolation gives a first estimate; repeating it (or a calculator's IRR function) gives the exact rate.
IRR ≈ 40 + 5·72.89/(72.89 − (−2 929.60)) = 40.12%
exact: NPV(40.12%) = 0 → IRR = 40.12%
Answer
IRR = 40.12%
29.Normal distribution
Answer: z = 1.17
From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.
Area to the left of z
Φ(z) = (1 + 0.7580)/2 = 0.8790
Read the z-table backwards
Find 0.8790 inside the table and read off z.
z = 1.17
Answer
z = 1.17
30.Normal distribution
Answer: x = 75.4 points
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) = 0.85
z from the table
z ≈ 1.04
Back to the original units
x = 65 + 1.04·10 = 75.4 points
Answer
x = 75.4 points
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