Summary of "Design and analysis of centrifugal compressor using Ansys Workbench | Bladegen | CFX"

Overview

Tutorial walkthrough showing an end-to-end design and CFD analysis of a centrifugal compressor using ANSYS Workbench together with external turbomachinery design and meshing tools. Goal: produce an impeller geometry and evaluate aerodynamic performance for a given specification.

Design specification (inputs)

Toolchain and workflow (step sequence)

  1. Preliminary design in VISTA CCD
    • Enter the design specifications to generate an initial impeller design.
  2. Import preliminary design into BladeGen (blade editor) to create and modify the impeller geometry.
    • Editable items: impeller flowpath and blade profiles, blade count, leading/trailing edge types, splitter blade position.
    • Span-wise control: blade angle progression and blade thickness progression across multiple span sections (4 sections shown).
    • Shape control via beta/angle programs and thickness controls.
    • Export impeller to various CAD/mesh file formats once satisfied.
  3. Mesh generation using the turbomachinery mesher (Turbo / TurboGrid / TGrid).
    • Demonstration used a coarse mesh for speed; mesh quality shown and discussed.
  4. Export mesh to ANSYS CFX (via Workbench).
  5. Set boundary conditions in turbo mode inside CFX setup.
    • Tip: ensure the flow arrow direction matches impeller rotation; if opposite, enter negative RPM.
  6. Solve with the CFX solver.
  7. Post-process results in CFX-Post.
    • Extract and tabulate major performance parameters (pressure rise, mass flow, efficiency, etc.).

Tip: Boundary-condition orientation matters for rotational sign. If the flow arrow is opposite the impeller rotation, use a negative RPM.

Key features & tips highlighted

Outputs shown

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