RIBES

Radial basis functions at fluid Interface Boundaries to Envelope flow results for advanced Structural analysis

 Coordinatore UNIVERSITA DEGLI STUDI DI ROMA TOR VERGATA 

 Organization address address: VIA ORAZIO RAIMONDO 18
city: ROMA
postcode: 173

contact info
Titolo: Prof.
Nome: Giuseppe
Cognome: Novelli
Email: send email
Telefono: 390673000000
Fax: 39067236609

 Nazionalità Coordinatore Italy [IT]
 Totale costo 292˙000 €
 EC contributo 219˙000 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2013-02
 Funding Scheme JTI-CS
 Anno di inizio 2014
 Periodo (anno-mese-giorno) 2014-12-01   -   2016-05-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    UNIVERSITA DEGLI STUDI DI ROMA TOR VERGATA

 Organization address address: VIA ORAZIO RAIMONDO 18
city: ROMA
postcode: 173

contact info
Titolo: Prof.
Nome: Giuseppe
Cognome: Novelli
Email: send email
Telefono: 390673000000
Fax: 39067236609

IT (ROMA) coordinator 219˙000.00

Mappa


 Word cloud

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

fem    meshes    cfd    structures    models    accurate    rbf    numerical    mapping    aircraft    exchange    millions    weight    loads    ribes    software   

 Obiettivo del progetto (Objective)

'In the framework of Clean Sky2, Green Regional Aircraft - GRA - will deliver low-weight aircraft using smart structures. With the aim of mitigating environmental impact through a substantial reduction of pollutant emissions and fuel consumption, a reliable numerical methodology is required to accurately optimise the weight. The design process implies using of CFD and FEM structural models. Then the object of the Area-01 - Low weight configurations requires, in particular, the development and validation of methodologies and software tools for the implementation of accurate transfer of loads between numerical models, to guarantee a safer design workflow that allows a reduction of uncertainties, gaining the goal of weight reduction. This problem poses a technological challenge especially for numerical models of complex aerospace structures where flow data exchange between non conformal CFD and FEM meshes, has to be performed on huge calculation models (several millions cells). The research project proposes an innovative approach for loads mapping based on Radial Basis Functions (RBF) theory and RIBES software implementation. A technology previously developed in the field of mesh morphing (RBF Morph™) capable to deal with large dataset (millions of points) will be used to enable an accurate mapping. The meshless nature of the method facilitates all the complex tasks needed to properly exchange information between meshes. The effectiveness of the approach will be demonstrated on an aeronautic wing structure by means of numerical and experimental checks and by a quantitative estimation of weight reduction obtained using the optimization module included in the RIBES application.'

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