1. Characteristics of Turbomachines Flashcards
What is the formula for meridional velocity V(m)
- V(m)^2 = V(x)^2 + V(r)^2
- V(x) = axial velocity
- V(r) = radial velocity
what is the continuity equation applied along a stream tube
- ρ V(m) 2pi r t = 𝑚̇ = const
- t = stream tube thickness
- r = local radius
what is an assumption we can use for axial machines to simplify their analysis
- r is constant
- so V(r) = 0 meaning V(m) = V(x)
what is the formula for the torque that the blades exert on the fluid T(f)
- T(f) = 𝑚̇(r(2)V(θ2) - r(1)V(θ1))
what is the formula for the torque that the fluid exerts on the blade and why
- T(b) = -T(f)
- because the torque on the blade is equal and opposite to that on the fluid
what is eulers work equation in terms of stagnation enthalpy h(0)
- h(0) - ΩrV(θ) = constant along a streamline
- Ω = blade/shaft speed
what is the formula for relative stagnation enthalpy h(0,rel)
- h(0,rel) = h + 1/2*V(rel)^2
what is the formula for V(θ,rel)
- V(θ,rel) = V(θ) - Ωr
what is the formula for V(rel)^2
V(rel)^2 = V(m)^2 + V(θ,rel)^2
what is eulers work equation in terms of relative stagnation enthalpy h(0,rel)
- h(0,rel) - 1/2Ω^2r^2 = constant along a streamline
what are the 5 scenarios that eulers work equation is valid for
- flow along any stream tube
- steady flow
- adiabatic flow
- viscous and inviscid flow
- torque provided by the blades only
what is eulers work equation in terms of power W(x)-dot
- W(x)-dot = 𝑚̇(U(2)V(θ2) - U(1)V(θ1))
what is the formula for the local speed of sound c
- c = sqrt(γRT)
what is the formula for the flow coefficient φ
- φ = V(m)/U
what is the formula for the loading coefficient Ψ
- Ψ = dh(0)/U^2
what is the formula for the loading coefficient Ψ if the radius is constant
- Ψ = dV(θ)/U
what is the formula for the reaction Λ and what kind of enthalpies are being used
- Λ = dh(rotor)/dh(stage)
- these are static enthalpies
considering the flow is usually nearly isentropic, what is an approximation for the reaction Λ
- Λ = dp(rotor)/dp(stage)
what does a reaction of 50% for axial turbomachinery imply
- the velocity triangles are symmetrical
- and the stator and rotor blades have similar shapes
what is the relationship between the reaction Λ across a rotor and a stator
Λ = dh(rotor)/dh(stage) = 1 - dh(stator)/dh(stage)
what is the formula for the reaction Λ in terms of the flow and loading coefficients
- Λ =1 - [1/2*φ^2]/[Ψ(tan^2(a2) - tan^2(a1))]
what do you need to remember about how to draw the rotors and stators for repeating axial compressors and turbines
- 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