泵轮、叶轮、螺旋桨等的叶片分析及飞机机翼空气动力学分析

NUMECA国际公司一直致力于高度集成及用户化的流场数值模拟软件，及其叶轮机械设计软件的研制和开发。这些软件均采用最新的先进数值分析技术。NUMECA国际公司集中了许多优秀的CFD工程师，他们可给用户提供及时有效的技术支持和服务。

Windows 64bit | + Docs & Tutorials | Size: 3.5 GB

Best-in-class turbomachinery design tools
Engineers looking to combine speed and accuracy for their virtual turbomachinery designs trust NUMECA for their toughest challenges.

We 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 segment 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 – confirming 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 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 (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
Multigrid 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 times gain in convergence speed
Embedded fluid structure interaction with the Modal and Flutter Analysis module
Multigrid 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 academic 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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