3. Preliminary Design Flashcards

1
Q

what is the specific speed

A
  • specific speed is a dimensionless group
  • whose numerical value is a means of deciding what type of machine is most suitable for an application
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2
Q

what is the formula for the volume flow rate, Q

A
  • Q = 𝑚̇/ρ
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3
Q

what is the incompressible expression for the flow coefficient, φ

A
  • φ = Q / ΩD^3
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4
Q

what is the incompressible expression for the stage loading coefficient, Ψ

A
  • Ψ = dp(0) / ρ Ω^2 D^2
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5
Q

what is the formula for the specific speed, N(s), aka the shape factor

A
  • N(s) = (𝑚̇/ρ_exit)^1/2 * Ω(dh_0)^-3/4
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6
Q

what is the specific speed and specific diameter mainly used for

A
  • choosing the type of machine at the preliminary design stage
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6
Q

what is the formula for the specific diameter, D(s)

A
  • D(s) = (dh_0)^1/4 * ρ_exit * D / 𝑚̇
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7
Q

for a repeating stage axial machine, what are the 4 conditions that are satisfied for it to work, using 1 rotor and stator stage for reference

A
  • V(x) = constant
  • a(1) = a(3)
  • V(1) = V(3)
  • the change in V(θ) through the rotor is equal and opposite to that through the stator
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8
Q

what is the formula for the stage loading coefficient in terms of the flow coefficient for a repeating axial machine, Ψ

A
  • Ψ = φ(tan(a2) - tan(a1))
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9
Q

what is the formula relating the flow coefficient and reaction to the stage loading coefficient, for a repeating axial machine Ψ

A
  • Ψ = 2(1 - Λ - φtan(a1))
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10
Q

what is the purpose of preliminary stage design

A
  • to fix the velocity triangles by choosing the values of three dimensionless groups
  • then by matching to the overall requirements, the layout of the machine can be determined
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11
Q

what are the variables that a designer must fundamentally fix in order to fix the velocity triangles for a repeating stage machine

A
  • three from a1, a2, b1 and b2
  • fixing 3 automatically fixes the other
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12
Q

rather than fixing a1, a2, b1 or b2 directly, which variables are better to fix

A
  • φ, Ψ and Λ
  • the missing flow angles can be found from other formulas relating them
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13
Q

what is the formula for the reaction, Λ, in terms of φ

A
  • Λ = 1 - φ/2(tan(a2) - tan(a1))
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14
Q

what is the formula for tan(β)

A
  • tan(β) = tan(a) - 1/φ
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15
Q

how are the fixed values for φ, Ψ and Λ chosen

A
  • from best practice and experience testing previous designs
  • typical values for each are explored later
16
Q

what is the formula for the number of stages, n(stage) and how are the variables determined

A
  • n(stage) = dh(0,overall) / (U^2 * Ψ)
  • dh(0,overall) is fixed by the operating requirements
  • U is determined by stress limits of operating requirements
17
Q

if the blade cross-section is constant from hub to tip, what is the formula for peak centrifugal stress in a rotor, σ

A
  • σ = ρ(b) Ω^2 A(x) / 2pi
18
Q

what is the formula for the annulus area, A(x), if the mass flow rate and flow coefficient is known

A
  • A(x) = 𝑚̇ / ρφU
19
Q

what is the formula for dh_0,stage if you can work out dh_0,machine and are told the number of stages N

A
  • dh_0,stage = dh_0,machine / N
20
Q

what are the three repeating stage conditions

A
  • Vx = constant
  • a1 = a3
  • V1 = V3
21
Q

for the reaction Λ = dh_rotor/dh_stage = 1 - dh_stator / dh_stage, what is dh_stage and dh_stator

A
  • dh_stage = u^2*Ψ
  • dh_stator = 1/2(V_2^2 - V_1^2)
22
Q

if the reaction is 0.5 in a repeating axial turbine stage, what is the relationship between the blade angles from a1 to a3 and b1 to b3

A
  • b3 = -a2
  • b2 = -a1
23
Q

what is zweifels expression Z in words

A
  • Z = actual blade force / ideal blade force
24
Q

when investigating blade loading and zweifels rule, what is the first plot you draw

A
  • V/V2 against axial distance
  • youre drawing the pressure and suction surface distributions for high pitch (s) and spacing (s/c), low pitch and optimum
25
Q

how does the blade loading vary with high and low blade pitch s

A
  • high pitch and spacing gives a high peak V
  • boundary layer loss is proportional to V^3 so this is high
  • low pitch and spacing gives a low peak V
  • but losses due to high wetted area
  • generally, as pitch increases blade loading increases
26
Q

what is the plot for showing the significance of the Z coefficient

A
  • Cp against x/Cx
  • Cp = p - p01 / p01 - p2
  • you draw the same shape of the PS and SS distributions and shade it in
  • but also with a rectangle from y = - to the end of the shaded plot
  • this rectangle represents ideal loading and the shaded is ideal
27
Q

what does Z actually indicate

A
  • the ideal loading is impossible because its a rectangle
  • so Z indicates the area of overshoot necessary to achieve loading
  • such that theres an optimum balance of loss due to wetted area and boundary layer loss