E-CFD-GPU

Efficient CFD Multi-physics programming research

 Coordinatore NUMERICAL MECHANICS APPLICATIONS INTERNATIONAL SA 

 Organization address address: CHAUSSEE DE LA HULPE 187-189
city: BRUXELLES
postcode: 1170

contact info
Titolo: Prof.
Nome: Charles
Cognome: Hirsch
Email: send email
Telefono: +32 2 642 28 01
Fax: +32 2 647 93 98

 Nazionalità Coordinatore Belgium [BE]
 Totale costo 150˙000 €
 EC contributo 112˙500 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2010-01
 Funding Scheme JTI-CS
 Anno di inizio 2011
 Periodo (anno-mese-giorno) 2011-02-01   -   2013-07-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    NUMERICAL MECHANICS APPLICATIONS INTERNATIONAL SA

 Organization address address: CHAUSSEE DE LA HULPE 187-189
city: BRUXELLES
postcode: 1170

contact info
Titolo: Prof.
Nome: Charles
Cognome: Hirsch
Email: send email
Telefono: +32 2 642 28 01
Fax: +32 2 647 93 98

BE (BRUXELLES) coordinator 67˙500.00
2    UNIVERSITAET GRAZ

 Organization address address: UNIVERSITAETSPLATZ 3
city: GRAZ
postcode: 8010

contact info
Titolo: Prof.
Nome: Gundolf
Cognome: Haase
Email: send email
Telefono: +43 316 380 5178
Fax: +43 316 380 9815

AT (GRAZ) participant 45˙000.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

cpu    configurations    parallel    transition    efforts    fidelity    simulation    computationally    convergence    chain    steady    extending    calculations    acceleration    pre    tools    gain    performance    software    magnitude    rans    hybrid    efficient    physics    environment    algorithms    orders    generation    turnaround    time    intensive    cfp    turn    gpu    aircraft    global    simulations    cad    cfd    booster    team    module   

 Obiettivo del progetto (Objective)

'The current evolution in the aeronautical field towards high-fidelity simulations, including multi-physics and more reliable modeling of turbulence and transition, calls for a new approach of the complete CFD-multi-physics simulation chain, with a drastic reduction of its turnaround time. This requires revising the whole CAE chain, from pre-processing (CAD handling and mesh generation), to very fast basic CFD algorithms and to efficient, full parallel post-processing, in order to achieve a reduction of the global turn-around time by several orders of magnitude. On a shorter term, of 24 months of the current CfP project, the following objectives can be ensured, based on very recent developments performed at NUMECA Int.: • A gain of one order of magnitude at the pre-processing level, covering automatic CAD cleaning, wrapping and parallel unstructured grid generation for arbitrary complex configurations with the software system HEXPRESS™/Hybrid. • A gain of one order of magnitude, due to a novel convergence acceleration algorithm, allowing calculations with CFL=1000 and convergence of steady state RANS simulations, in 50 multigrid cycles. The present proposal has as objective to respond to the CfP topic by • extending these capabilities to the GRA-LNC configurations • extending the convergence acceleration methodology to simulations with laminar-turbulent transition, and to unsteady flows • providing guidelines for a next generation software environment for industrial aerodynamics simulation, in response to task 2 of the CfP, • porting of the CFD code and the convergence acceleration algorithms to GPU’s, with an expected additional gain of 1 to 2 orders of magnitude. One could therefore expect, combining the above mentioned efforts that within the framework of the project duration, a gain of 3-to 4 orders of magnitude will be achieved, in global CPU performance and turn-around time, for steady state RANS simulations in a first step.'

Introduzione (Teaser)

Over the last decades, computational fluid dynamics (CFD) has become widely accepted as the main method for evaluating the aerodynamic performance of new designs. EU-funded researchers have proposed a new approach to drastically reduce the turnaround time of such high-fidelity simulations.

Descrizione progetto (Article)

CFD tools are increasingly used in the early phases of design because of their reliability and higher flexibility. Tremendous progress in the physical modelling of airflow, numerical algorithms and computer power is exploited for the design of aircraft and cars. But this is not the end of the story.

CFD simulations are computationally intensive. The simulation of a car or an aircraft in landing configuration requires geometry defined by thousands of surfaces, discretised with hundred millions of elements. Comparing various alternatives for enabling faster research using CFD was the aim of the EU-funded project E-CFD-GPU (Efficient CFD multi-physics programming research).

Tools such as HexpressTM/Hybrid designed for meshing complex geometries, the CPU Booster convergence acceleration module and its extension allowed impressive improvements in different stages of the computation chain. For instance, acceleration with the CPU Booster TM module can provide up to five times gain in convergence speed.

General-purpose graphics processing unit (GPU) technology was also explored to accelerate computationally intensive calculations. The capability of GPUs to simulate the flow behaviour of complex fluids was demonstrated by the pioneering work of the E-CFD-GPU team.

Finally, significant efforts were devoted to simplifying the simulation environment. Among the project outcomes were efficient algorithms developed for a multi-user, multi-physics simulation platform that takes advantage of modern hardware architectures. The E-CFD-GPU team are confident that these enhancements in CFD software will have a major impact on European competitiveness.

Altri progetti dello stesso programma (FP7-JTI)

METPROCELL (2011)

Innovative fabrication routes and materials for METal and anode supported PROton conducting fuel CELLs

Read More  

STRAINWISE (2010)

Hardware & Software Development of Wireless Sensor Network Nodes for Measurement of Strain in Airborne Environment

Read More  

MAESTRO (2011)

MembrAnEs for STationary application with RObust mechanical properties

Read More