Sfoglia per Autore  

Opzioni
Mostrati risultati da 1 a 10 di 10
Titolo Data di pubblicazione Autori File
Assessment of laminar-turbulent transition models for turbomachinery flow computations 1-gen-2005 L. CutroneP. De PalmaG. PascazioM. Napolitano
A flamelet/progress-variable approach for the simulation of turbulent combustion of real gas mixtures 1-gen-2008 Cutrone LDe Palma PPascazio GNapolitano M
A RANS flamelet-progress-variable method for computing reacting flows of real-gas mixtures 1-gen-2010 Cutrone, L.De Palma, P.Pascazio, G.Napolitano, M.
3D nozzle flow simulations including state-to-state kinetics calculation 1-gen-2014 Cutrone LPascazio G +
Numerical investigation of high-pressure combustion in rocket engines using flamelet/progress-variable models 1-gen-2015 COCLITE, AlessandroCUTRONE, LUIGIDE PALMA, PietroPASCAZIO, Giuseppe
Computing supersonic non-premixed turbulent combustion by an SMLD flamelet progress variable model 1-gen-2016 COCLITE, AlessandroCUTRONE, LUIGIDE PALMA, PietroPASCAZIO, Giuseppe +
The role of presumed probability density functions in the simulation of nonpremixed turbulent combustion 1-gen-2016 Coclite APascazio GDe Palma PCutrone L
An MPI-CUDA approach for hypersonic flows with detailed state-to-state air kinetics using a GPU cluster 1-gen-2017 Bonelli, FrancescoTuttafesta, MicheleCutrone, LuigiPascazio, Giuseppe +
Numerical Investigation of High Enthalpy Flows 1-gen-2017 Bonelli, F.Cutrone, L.Pascazio, G. +
State-to-state kinetics in CFD simulation of hypersonic flows using GPUs 1-gen-2019 Giuseppe PascazioFrancesco BonelliLuigi Cutrone +
Mostrati risultati da 1 a 10 di 10
Legenda icone

  •  file ad accesso aperto
  •  file disponibili sulla rete interna
  •  file disponibili agli utenti autorizzati
  •  file disponibili solo agli amministratori
  •  file sotto embargo
  •  nessun file disponibile