1. Characteristics of Turbomachines Flashcards

1
Q

What is the formula for meridional velocity V(m)

A
  • V(m)^2 = V(x)^2 + V(r)^2
  • V(x) = axial velocity
  • V(r) = radial velocity
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2
Q

what is the continuity equation applied along a stream tube

A
  • ρ V(m) 2pi r t = 𝑚̇ = const
  • t = stream tube thickness
  • r = local radius
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3
Q

what is an assumption we can use for axial machines to simplify their analysis

A
  • r is constant
  • so V(r) = 0 meaning V(m) = V(x)
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4
Q

what is the formula for the torque that the blades exert on the fluid T(f)

A
  • T(f) = 𝑚̇(r(2)V(θ2) - r(1)V(θ1))
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5
Q

what is the formula for the torque that the fluid exerts on the blade and why

A
  • T(b) = -T(f)
  • because the torque on the blade is equal and opposite to that on the fluid
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6
Q

what is eulers work equation in terms of stagnation enthalpy h(0)

A
  • h(0) - ΩrV(θ) = constant along a streamline
  • Ω = blade/shaft speed
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7
Q

what is the formula for relative stagnation enthalpy h(0,rel)

A
  • h(0,rel) = h + 1/2*V(rel)^2
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8
Q

what is the formula for V(θ,rel)

A
  • V(θ,rel) = V(θ) - Ωr
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9
Q

what is the formula for V(rel)^2

A

V(rel)^2 = V(m)^2 + V(θ,rel)^2

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9
Q

what is eulers work equation in terms of relative stagnation enthalpy h(0,rel)

A
  • h(0,rel) - 1/2Ω^2r^2 = constant along a streamline
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10
Q

what are the 5 scenarios that eulers work equation is valid for

A
  • flow along any stream tube
  • steady flow
  • adiabatic flow
  • viscous and inviscid flow
  • torque provided by the blades only
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11
Q

what is eulers work equation in terms of power W(x)-dot

A
  • W(x)-dot = 𝑚̇(U(2)V(θ2) - U(1)V(θ1))
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12
Q

what is the formula for the local speed of sound c

A
  • c = sqrt(γRT)
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13
Q

what is the formula for the flow coefficient φ

A
  • φ = V(m)/U
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14
Q

what is the formula for the loading coefficient Ψ

A
  • Ψ = dh(0)/U^2
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15
Q

what is the formula for the loading coefficient Ψ if the radius is constant

A
  • Ψ = dV(θ)/U
16
Q

what is the formula for the reaction Λ and what kind of enthalpies are being used

A
  • Λ = dh(rotor)/dh(stage)
  • these are static enthalpies
17
Q

considering the flow is usually nearly isentropic, what is an approximation for the reaction Λ

A
  • Λ = dp(rotor)/dp(stage)
18
Q

what does a reaction of 50% for axial turbomachinery imply

A
  • the velocity triangles are symmetrical
  • and the stator and rotor blades have similar shapes
19
Q

what is the relationship between the reaction Λ across a rotor and a stator

A

Λ = dh(rotor)/dh(stage) = 1 - dh(stator)/dh(stage)

20
Q

what is the formula for the reaction Λ in terms of the flow and loading coefficients

A
  • Λ =1 - [1/2*φ^2]/[Ψ(tan^2(a2) - tan^2(a1))]
21
Q

what do you need to remember about how to draw the rotors and stators for repeating axial compressors and turbines

A
  • the rotor blades are always going up
  • the stator blades are always going down
  • the compressor has rotor then stator
  • the turbine has stator then rotor