NUMECA FINE-Turbo 17.1 x64

[FaridKhan]

NUMECA FINE-Turbo 17.1 (x64)

[center][img]https://i.postimg.cc/nzxBQtcd/NUMECA-FINE-Turbo-17-1-x64.png[/img][/center]

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[center]Win/Linux | File Size: 3.2 GB[/center]

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[quote]Flow Integrated Environment for rotating and non-rotating flow analysis in external and internal turbomachinery applications. Recognized as the fastest and most accurate CFD suite by the worldwide turbomachinery community.
FINE™/Turbo is the fastest CFD suite for rotating machinery with incompressible and compressible fluids, from subsonic to hypersonic flow regimes. All types of multi-stage axial, radial or mixed-flow configurations are supported: compressors, turbines, pumps, fans, propellers or contra-rotating propellers. From meshing to results visualization, the FINE™/Turbo application-oriented graphical user interface is intuitive, enabling fast project set-up and analysis. The simulation process is streamlined with
AutoGrid5™: Automated grid generator for turbomachinery configuration, delivers the highest quality structured meshes with minimum user input. Its Wizard mode handles all types of rotating machinery configurations and complexities.
FINE™/Turbo flow solver: 3D Navier-Stokes flow solver, recognized as the fastest and most accurate for turbomachinery configurations. Acceleration of several orders of magnitude is achieved thanks to the CPU Booster™ technique, NLH approach, GPU acceleration and HPC scalability.
CFView™: Advanced post-processing tool, provides dedicated flow visualization and analysis outputs in an easy-to-use turbomachinery-oriented mode.
[b]Key features[/b]
AutoGrid5™: 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
FINE™/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 times 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 time
Cross-out high performance computing on supercomputers with linear speed-up on up to 5,000 to 10,000 cores
Embedded fluid structure interaction 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
Static pressure contour at 50% span of an impeller-diffuser configuration
Static pressure contour at 50% span of an impeller-diffuser configuration
Blade to blade cut of axial velocity field of a contra-rotating marine propeller
Blade to blade cut of axial velocity field of a contra-rotating marine propeller
Turbo fan engine - Courtesy Price Induction
Turbo fan engine - Courtesy Price Induction
Wind turbine blade
NLH simulation on Rotor 67 with 175 million grid cells per passage - Courtesy of Ramgen Power Systems
NLH simulation on Rotor 67 with 175 million grid cells per passage - Courtesy of Ramgen Power Systems
Multigrid convergence acceleration
Full Non-Matching Boundaries capability
Laminar-turbulent transition
Congugate heat transfers
Cavitation
Python scripting technology
CFView™
Multi-projects and multi-views graphical user interface
Specific turbomachinery visualization mode
Python scripting technology

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HomePage :

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