Cryogenic rocket engines, advanced gas turbines and diesel engines are characterized by the injection of a liquid fuel into a high temperature and pressure chamber. Typically the fuel is injected at high enough pressure to be close or above the critical pressure. In these conditions the behavior of the fluid differs strongly from that of a perfect gas. It exhibits large variations of thermodynamic and transport properties also for small temperature changes, with significant effects on mixing and combustion processes. In this context an appropriate numerical simulation should take into account such thermodynamic phenomena via suitable equation of state and transport properties relations.
DNS of a variable density jet in the supercritical thermodynamic state / Battista, F.; Picano, F.; Troiani, G.; Casciola, C. M.. - 15:(2011), pp. 303-308. ((Intervento presentato al convegno 8th International Conference on Direct and Large-Eddy Simulation, 2010 tenutosi a Eindhoven, NETHERLANDS [10.1007/978-94-007-2482-2_48].
Titolo: | DNS of a variable density jet in the supercritical thermodynamic state | |
Autori: | ||
Data di pubblicazione: | 2011 | |
Serie: | ||
Citazione: | DNS of a variable density jet in the supercritical thermodynamic state / Battista, F.; Picano, F.; Troiani, G.; Casciola, C. M.. - 15:(2011), pp. 303-308. ((Intervento presentato al convegno 8th International Conference on Direct and Large-Eddy Simulation, 2010 tenutosi a Eindhoven, NETHERLANDS [10.1007/978-94-007-2482-2_48]. | |
Handle: | http://hdl.handle.net/11573/1445986 | |
ISBN: | 978-94-007-2481-5 978-94-007-2482-2 | |
Appartiene alla tipologia: | 04b Atto di convegno in volume |
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