Skip to main content

Dimensionless parameters and their significance

Short answer

Flow coefficient φ = Q/(ND³) relates meridional velocity to blade speed. Head coefficient ψ = gH/(N²D²) indicates loading. Power coefficient λ = P/(ρN³D⁵). Reynolds number Re = ρND²/μ governs viscous effects. Mach number Ma = ND/a indicates compressibility. Specific speed N_s = N√Q/(gH)^(3/4) determines machine type (low N_s radial, high N_s axial).

Explain the dimensionless parameters used for turbomachines (flow coefficient, head or pressure coefficient, power coefficient, Reynolds number, Mach number and specific speed) and state the physical significance of each.

Dimensional analysis of a turbomachine (variables: DD, NN, ρ\rho, μ\mu, QQ, gHgH, PP) gives dimensionless groups that allow geometrically similar machines to be compared and model test results to be scaled up.

ParameterExpressionPhysical significance
Flow coefficientϕ=QND3\phi = \dfrac{Q}{N D^3}Proportional to the ratio of axial (meridional) velocity to blade speed. Fixes the shape of the velocity triangles
Head (pressure) coefficientψ=gHN2D2\psi = \dfrac{gH}{N^2 D^2}Ratio of head (energy per unit mass) to the kinetic energy based on blade speed. Measures the loading of the machine
Power coefficientλ=PρN3D5\lambda = \dfrac{P}{\rho N^3 D^5}Power per unit of ρN3D5\rho N^3 D^5; with ϕ\phi and ψ\psi it gives the efficiency η=ϕψ/λ\eta = \phi\psi/\lambda
Reynolds numberRe=ρND2μRe = \dfrac{\rho N D^2}{\mu}Ratio of inertia to viscous forces; controls friction loss. Its effect is small at high ReRe
Mach numberMa=NDaMa = \dfrac{ND}{a}Blade speed to speed of sound; important for compressors and gas turbines, where compressibility and shock losses appear
Specific speedNs=NQ(gH)3/4N_s = \dfrac{N\sqrt{Q}}{(gH)^{3/4}}Speed of a geometrically similar machine delivering unit flow at unit head. Decides the type: low NsN_s radial, high NsN_s axial

Use in practice

  1. Similarity: two machines are dynamically similar if ϕ\phi and ψ\psi (and ReRe, MaMa) are equal, and their efficiencies are then equal.
  2. Scaling laws: for the same fluid and constant ϕ\phi: Q∝ND3Q \propto N D^3, H∝N2D2H \propto N^2 D^2, P∝N3D5P \propto N^3 D^5.
  3. Selection of type: a high NsN_s means large flow and low head, which needs an axial machine; a low NsN_s means small flow and high head, which needs a radial one.
  4. Performance prediction: a single non-dimensional curve of ψ\psi and η\eta against ϕ\phi represents a whole family of machines.

For compressible flow, the mass flow parameter m˙T01/p01\dot m \sqrt{T_{01}}/p_{01} and the speed parameter N/T01N/\sqrt{T_{01}} are used in place of ϕ\phi and NN.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Turbo Machines chapter 1 questions →