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10/25/2009
On October 25, 2009, Advanced Dynamics Corporation released the Word's first multi-disciplinary, multi-physics, multi-scale and multi-fidelity analysis amd design optimization (4MAO) ...... |
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For immediate inquiries call Tel: (859) 699-0441 Fax:(859) 243-5615 Email: Contact@advanceddynamics-usa.com |
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ASTE-P
All Necessary Components for Multi-disciplinary Analysis and Design of Aerospace, Automotives, Marine Ships and Complex Mechanical Systems Are Included in One Package of Software - ASTE-P 2.0
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10 Advantages of ASTE-P Compared to Existing CAE Software such Fluent, CFX, Nastran and Ansys:
1¡¢Integrated, user-friendly and self-contained 10 modules of all necessary components for multi-disciplinary analysis and design of aerospace, automotives, marine ships and complex mechanical systems: CFD, CSD, FSI &AE, ASE, Propulsion, CAA, Material Database, Particle Methods and Pre-processor and Post-processor. All modules can be RUN and BOUGHT individually or jointly with other nodule(s).
2¡¢Strong capability for solving nonlinear problems for fluid dynamics (i.e. shock, flow separation, high-temperature gas dynamics), structural dynamics (i.e. crack, impact and penetration and arbitrary large deformations using particle-based methods) and coupled nonlinear fluid-structure interaction (FSI) and aeroelasticity/Aeroservoelasticity (AE/ASE) (i.e. flutter/LCO, buffet).
3¡¢Strong capability for solving fluid-structure interaction, aeroelasticity and aeroservoelasticity problems, the CFD and CSD solvers are directly embedded into FSI/AE and ASE modules and no third party software is need, both grid-based and particle-based approaches are available in FSI/AE and ASE modules for solving viscous, large deformation and strong nonlinear problems.
4¡¢Mesh generation is not needed for complex and or rotating geometry (i.e. full aircraft, rotating problems such as rotor wake interacting with fuselage, turbine blade and disk) if particle method is used.
5¡¢Faster turn-round time is guaranteed by using reduced order models (ROM) such as Proper Orthogonal Decomposition (POD), Volterra ROM (e.g. 2 hours coupled CFD/CSD simulation vs. 2 seconds for POD-ROM for a flutter analysis of a typical 3D wing)
6¡¢Higher numerical accuracy is achieved by incorporating most recent numerical algorithms in CFD and CSD for high Mach number in ASTE-P (Mach number could be as high as 50) and incompressible flows with velocity approach to 0, and multiphase flows with essentially no-upper limit for number of dispersed phases.
7¡¢Simulation data is directly outputted for design optimization.
8¡¢Strong capability for computing combustion and noise (for both subsonic and supersonic jets).
9¡¢Independent pre- and post- processors for geometry modeling, mesh and particle generations and structural, unstructural and particle data high-quality display and fast animation capability (e.g. fast vibration of structural component).
10¡¢Comprehensive and user-friendly material database for user to choose and customize the materials types and properties. |
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