Rapid Turbomachineary Design - AxSTREAM
Axial Compressor
Key Features and Benefits
- The scope of axial compressor design and analysis: flow path with normal (rotor-stator) and single row stages, mixed flow (axial/radial) flow path, multi-section flow path, flow path with counter-rotating rotors.

- Axial compressor flow path preliminary design/sizing/optimization, choosing the optimal number of compressor stages and cascade angles.


- Multistage flow path meanline analysis and optimization with support of “as-designed” and “off-design” operational conditions.
- Meanline analysis of combined axial-radial compressor flow path.
- Turbomachinery flow path throughflow analysis and stage throughflow analysis with search for optimal blade twist using the optimization methods through design cycle in the interactive mode.
- Axial compressor analysis and optimization in the “off-designed” mode using the integrated optimizer based on the design-of-experiment (DoE) methodology.
- Performance map generation including flow path of variable geometry: vanes/blades rotation schedules.
- Generation, interactive editing, and optimization of the cascades. Flow and boundary layer calculation.
- 3D airfoil design in the automatic and interactive modes with geometric and strength criteria monitoring; 3D fan and compressor blade design with custom lean and sweep.
- Custom profiles database.
- Reusable axial compressor stages libraries.
- Experimentally confirmed empiric and custom loss models.
- Embedded fluids library with custom extension option.
- Embedded material library with custom extension option.
- Export of 3D blade geometry for detailed CFD analysis to NUMECA, CFX, and Fluent solvers; export of properties of fluids in a table for CFD analysis to CFX™.
- Export of 3D blade geometry to CAD in IGES formats.
- Express structural and modal axial compressor airfoil analysis via the embedded FEA module with automatic mesh generation.
- Express 3D flow analysis via the embedded FEA potential flow solver with automatic mesh generation.
- Detailed Mollier diagram.
- Charts for blade loading on Profiling and AxFLOW (Eulier).
- Availability of section of 3D domain (AxSTRESS, AxFLOW), Campbell diagram (AxSTRESS).
- 1D/2D Streamline solver allows finding compressor surge, stall and choke. It is capable to calculate transonic and subsonic stages of compressor
- AxMAP helps develop compressor map and can show dependence of pressure ratio of mass flow and rotation speed.