The Hong Kong Polytechnic UniversityDepartment of Aeronautical and Aviation Engineering

04 / TRANSFER · Propulsion

Compressor Velocity Triangles

Cycle & componentsBrowser calculation

Unwrap a rotor at one radius. Change the swirl and see shaft work become total-temperature and pressure rise.

TURN THE FLOW. TRANSFER WORK.LIVE B
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Steady calculation · adjust the controls to compare states

Both velocity triangles use the same scale. C = W + U. Turquoise: absolute C; pink: relative W; amber: blade U. No blade shape, incidence, stall or surge prediction is made.

A · no saved reference
01 / NOTICE THE CHANGE

Separate the frames

Absolute velocity C belongs to the stationary frame. Relative velocity W is what a moving blade sees. Their difference is blade speed U.

02 / NOTICE THE CHANGE

Remove swirl without adding work

The idealised stationary stator removes outlet swirl and raises static temperature. Total temperature remains unchanged through it.

03 / NOTICE THE CHANGE

Change efficiency independently

For a fixed velocity triangle, work and total-temperature rise stay fixed. Lower stage efficiency gives less total-pressure rise.

CALCULATED FROM THE SAME MODEL

Read the parameter study

B · solid turquoise   A · dashed amber
Dots mark the selected settings; curves sweep one variable

Compare the evidence

QuantityA · savedB · liveUnit

A remains fixed until you save again. Export includes settings, selected outputs and curve data.

Equations, assumptions and topic connections

Physical model

Steady mean-line constant-radius compressor energy account. Constant axial velocity, cp = 1005 J/(kg K), γ = 1.4, inlet total temperature 300 K. Rotor adds prescribed swirl; stator returns swirl to zero with unchanged total enthalpy. A selected overall stage efficiency determines total-pressure ratio. No radial equilibrium or compressor map is claimed.

Δht = U(Cθ₂ − Cθ₁); ΔTt = Δht/cp; PR = [1 + η Δht/(cpTt₁)]^(γ/(γ−1)). T = Tt − C²/(2cp). At 10 kg/s and mean radius 0.25 m, torque = ṁrΔCθ and shaft power = torque × U/r.

Topic connections

S10 · Subsystems 02, PDF pp. 15–26; candidate diagrams pp. 18–24. This connects velocity triangles to compressor work and cycle analysis. Original vector diagrams.

MIT · energy exchange with moving blades

Original schematic diagrams. No manufacturer performance, certification or maintenance-authorisation claim. Numerical verification checks the declared model; it is not experimental validation. Model version: course-foundations-v1.

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