NSHOCK

Non classical rarefaction shock-waves in molecularly complex vapours

 Coordinatore POLITECNICO DI MILANO 

Spiacenti, non ci sono informazioni su questo coordinatore. Contattare Fabio per maggiori infomrazioni, grazie.

 Nazionalità Coordinatore Italy [IT]
 Totale costo 1˙485˙600 €
 EC contributo 1˙485˙600 €
 Programma FP7-IDEAS-ERC
Specific programme: "Ideas" implementing the Seventh Framework Programme of the European Community for research, technological development and demonstration activities (2007 to 2013)
 Code Call ERC-2013-CoG
 Funding Scheme ERC-CG
 Anno di inizio 2014
 Periodo (anno-mese-giorno) 2014-03-01   -   2019-02-28

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    POLITECNICO DI MILANO

 Organization address address: PIAZZA LEONARDO DA VINCI 32
city: MILANO
postcode: 20133

contact info
Titolo: Dr.
Nome: Alberto
Cognome: Guardone
Email: send email
Telefono: +39 02 2399 8393
Fax: +39 02 2399 8334

IT (MILANO) hostInstitution 1˙485˙600.00
2    POLITECNICO DI MILANO

 Organization address address: PIAZZA LEONARDO DA VINCI 32
city: MILANO
postcode: 20133

contact info
Titolo: Dr.
Nome: Francesco Giovanni
Cognome: Cecchet
Email: send email
Telefono: +39 02 2399 8331
Fax: +39 02 2399 8334

IT (MILANO) hostInstitution 1˙485˙600.00

Mappa


 Word cloud

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

flow    supersonic    regimes    vapour    eighteen    molecularly    divergent    real    expansion    gasdynamics    gases    configurations    nozzle    flows    compression    fluids    siloxanes    mixtures    subsonic    gas   

 Obiettivo del progetto (Objective)

'The expansion of a dilute gas through a gasdynamics convergent-divergent nozzle can occur in three different regimes, depending on the inlet and discharge conditions and on the gas: via a fully subsonic expansion, via a subsonic-supersonic or via a subsonic-supersonic-subsonic expansion embedding a compression shock wave within the divergent portion of the nozzle. I devised an exact solution procedure for computing nozzle flows of real gases, which allowed me to discover that in molecularly complex fluids eighteen additional different flow configurations are possible, each including multiple compression classical shocks as well as non classical rarefaction ones. Modern thermodynamic models indicate that these exotic regimes can possibly occur in nozzle flows of molecularly complex fluids such as hydrocarbons, siloxanes or perfluorocarbons operating close to the liquid-vapour saturation curve and critical point. The experimental observation of one only of these eighteen flow configurations would be sufficient to prove for the first time that non classical gasdynamics phenomena are indeed possible in the vapour region of a fluid with high molecular complexity To this purpose, a modification to the blow-down wind tunnel for dense gases at Politecnico di Milano is proposed to use mixtures of siloxane fluids. Measurements are complemented by numerical simulations of the expected flow field and by state-of-the-art uncertainty quantification techniques. The distinctive feature of the proposed experiment is the adoption of mixture of siloxanes as working fluids. Mixtures of siloxanes are well known to exhibit an higher stability limit than their pure components, due to the redistribution process occurring at high temperature. The increased understanding of real-gas dynamics will enable to improve the design of Organic Rankine Cycle Engines, to be used in small scale energy production from biomasses, binary geothermal systems and concentrating solar thermal power plants.'

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