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ptucb1990 · Senior Joined: 11 Jun 2013 Posts: 4964

NUMECA FINE Turbo 9.0-3 x86/x64 NUMECA FINE Turbo 9.0-3 x86/x64

NUMECA FINE?Turbo 9.0-3 x86/x64 | 2.46 GB

Program FINE / Turbo - the world's first settlement CAE software package (PC) High-level solution-oriented specialized tasks turbomachinery CFD and turbomachinery .

Complex structure FINE / Turbo:

AutoBlade: parametric oscillator blade rows ;

AutoGrid: parametric block structured automatic mesh generator for turbomachinery ;

IGG: block structured grid generator for arbitrary geometry ;

Euranus: structured 3D solver of the Navier -Stokes equations ;

CFView: postprocessor .

AutoBlade - parametric oscillator blade rows , allows the engineer to quickly confecționate and instantly upgrade the flow part of the turbomachine , working with in terms of turbomachinery ( chord angles of entry, exit , throat , etc.) .

AutoGrid - automatic block- structured mesh generator , is inextricably linked with AutoBlade.

This connection allows to parameterize not only geometric but also grid tip , which in turn makes it possible to build a PC NUMECA into the overall design of the entire enterprise. AutoGrid can create parametric grid models blades with all the features - blowing cooling air shroud , gaps , etc.

Euranus - calculation module ( solver ) . By virtue of a structured approach and options multigrid (nested grid ) solution is obtained in 3-5 times faster than any other universal CFD package. This requires 2.3 times less memory.

Unique solutions for NUMECA joint calculation of movable and fixed settlement areas is aimed to obtain quick solutions for the unsteady multistage machines with distinct periodic boundaries. Including it is possible to explore the Clocking Effect.

Also become traditional for joint calculations of rotor and stator methods:

Mixing Plane ( Surface Melting Pot )

Frozen Rotor (� Stopped " Rotor )

Implemented as unique for generic PC CFD methods :

Domain Scaling Method ( scaling method )

Phase Lagged Method ( Generalized Space- Time Periodic Boundary Conditions )

As well as a unique method for CFD approaches :

Non Linear Harmonic ( Methods of Nonlinear Harmonic Analysis)

This approach is used to quickly obtain an accurate solution for unsteady multistage turbomachinery .

Simplified methods of analysis of flow in the flow section �Throughflow Model� and �Blade to Blade Module� serve to quickly assess the quality of the flow in the blade rows and the distribution of the flow of the blade height .

Unique custom module to create a block- structured grid allows you to create parametric models blades with all the features - blowing cooling air shroud , clearances, etc. ..

IGG - block structured grid generator for arbitrary geometry . Powerful and flexible environment for building high-quality discrete models . Implemented efficient algorithms for smoothing multiblock grids. User system creating scripts greatly simplifies and automates the generation of grids for standard elements .

CFView - a powerful visualization platform solutions , provides a full range of options for displaying the qualitative and quantitative characteristics 2D/3D calculations.

Areas of application:

PC FINE / TurboTM - used to solve practical problems of fluid dynamics in the design and optimization of all types of turbomachinery ( turbomachinery ) multistage axial , radial and mixed compressors, turbines , pumps, fans and propellers , as well as snails, diffusers , heat exchangers and exhaust systems.