NUMECA FINE/Turbo 16.1

Best-in-class turbomachinery design toolsWe have designed a unique toolset that encompasses a complete end-to-end solution: 1D to 3D, Meshing, CFD and Optimization, all in one single environment. Thanks to more than 75 years of expertise in rotating machinery, the environment displays an unsurpassed ease-of-use and accuracy.

Configurations range from multi-stage axial to radial to mixed-flow configurations (compressors, turbines, pumps, fans, propellers or contra-rotating propellers).

Key Features

Meanline design

For all major turbomachinery configurations. Meanline options include:

COMPAL for radial and mixed-flow compressors

PUMPAL for radial, mixed-flow, axial pumps

RITAL for radial and mixed-flow turbines

AXIAL for axial compressors and turbines

Detailed 3D design

For geometry and blading using AxCent, including throughflow, 2D blade to blade and streamline curvature calculation.

2D and radial blading

Agile links to COMPAL, PUMPAL, RITAL,AXIAL, OMNIS/Turbo, pbFEA and MAX-PAC

Bezier-based cross-section (axial) and geometry generation (radial)

Blade generation sheets

Blade lean

CAD output (IGES, STEP, ACIS, Parasolid, STL)

Circular-arc and line snt contours

Fillets (single-radious, variable, elliptical)

Ideal and real fluids

Independent hub and shroud

Multistreamtube (MST) calculation for both compressible and incompressible flow

Radial stacking of up to 3-cross-sections at LE, TE or CG

Rapid loading calculation for both compressible and incompressible flow

Single-blade raw capability

Suitable for compressors, fans, pumps and turbines

Swept leading and trailing edges

Throat area calculation

Add: BANIG

Add: Blade stacking of 2 to unlimited number of cross sections

Enhanced flank milling - config ruled surface

Flow cuts and trims/extensions

Flow injection and extraction

Inlet boundary layer calculations

Non-axisymmetric walls

Parameterized blade types (MCA, DCA, Pritchard, Enhanced Pritchard)

Parameterized blade types (NACA, Constant Passage, simple airfoil)

Simple and independently-specified splitter blades (Independent was option)

Stacking curve adjustment in meridional and tangential directions

OMNIS/AutoGrid

Parallel Mesh Generation

Wizard mode: optimal mesh topology based on configuration

Advanced geometry features: blade fillets, cooling systems, axisymmetric and non-axisymmetric effects

Advanced configurations: multistage, bulb, unshrouded and by-pass

Automated blocking and meshing of axisymmetric effects

Python scripting technology

OMNIS/HEXPRESS

Full Hexahedral Grids (no prism, no tetrahedra, no pyramid)

Direct CAD import capabilities

CAD manipulation and decomposition tools

Mesh wizard for rapid solution set-up and easy back and forth operation

Buffer cell and boundary layer insertion for high quality cells in boundary layer regions

Automatic refinement procedures based on user defined sensors either next to solid walls or at specified area in the domain

Multi domain capabilities allowing the treatment of CHT and multi-part geometry models

Full non-matching multi-block connection, allowing multi-row turbomachinery meshing

OMNIS/Turbo flow solver

One single code for all types of fluids (incompressible, perfect or real gas, compressible liquid and condensable) and speed (low speed to hypersonic regime)

Acceleration with the CPU Booster module provides 3-5 s gain in convergence speed

Non Linear Harmonic (NLH) module for full unsteady rotor-stator interactions with gains of 1 to 3 orders of magnitude in CPU

Cross-out High Performance Computing (HPC) on supercomputers with linear speed-up on up to 5,000 to 10,000 cores

Embedded Fluid Structure Interaction (FSI) with the Modal and Flutter Analysis module

Uncertainty Quantification module to study the variability with respect to geometrical or operational uncertainties

Automated performance curve creation

Mulid convergence acceleration

Full Non-Matching Boundaries capability

Laminar-turbulent transition

Congugate heat transfers

Cavitation

Python scripting technology

OMNIS/Open-DBS flow solver

One single code for all types of fluids (incompressible, low-compressible, condensable and fully compressible) and speed (low speed to hypersonic regime)

Acceleration with the CPU-Booster module provides 3-5 s gain in convergence speed

Embedded fluid structure interaction with the Modal and Flutter Analysis module

Mulid convergence acceleration

Multidomain capability

Combustion

Radiation

Lagrangian multiphase

Cavitation

Multispecies reacting flows

Thermodynamics tables and combustion tables generation

Python scripting technology

OpenLabs

OpenLabs allows users to customize or add physical models

Flexible and user-friendly Graphical User Interface

Users don't need to care about programming details and code structure

OpenLabs can be used in a wide variety of industrial and acad applications

Identical computing and memory costs compared to source-coded models

Free access to all OMNIS/Open community

OMNIS/Post

Multi-projects and multi-views graphical user interface

Python scripting technology

Surface and 3D local value

Iso-lines

Color contour

Vector

Iso-surfaces

Cloud of particles

Line chart

Integral

Formula and operator derived quantities

Live co-processing



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