• français
    • English
    English
  • Ouvrir une session
Aide
Voir le document 
  •   Accueil de SAM
  • Dynamique des Fluides (DynFluid)
  • Voir le document
  • Accueil de SAM
  • Dynamique des Fluides (DynFluid)
  • Voir le document
JavaScript is disabled for your browser. Some features of this site may not work without it.

Study on the Resolution of Large-Eddy Simulations for Supersonic Jet Flows

Conférence invitée
Auteur
JUNQUEIRA-JUNIOR, Carlos
134975 Laboratoire de Dynamique des Fluides [DynFluid]
F. ABREU, Diego
471029 Instituto Tecnológico de Aeronáutica [São José dos Campos] [ITA]
T. V. DAURICIO, Eron
471029 Instituto Tecnológico de Aeronáutica [São José dos Campos] [ITA]
F. AZEVEDO, João Luiz

URI
http://hdl.handle.net/10985/22736
DOI
10.2514/6.2022-3327
Date
2022-06

Résumé

The present study is concerned with large-eddy simulations (LES) of supersonic jet flows. The work addresses, in particular, the simulation of a perfectly expanded free jet flow with an exit Mach number of 1.4 and an exit temperature equal to the ambient temperature. Calculations are performed using a nodal discontinuous Galerkin method. The present effort studies the effects of mesh and polynomial refinement on the solution. The present calculations consider computational meshes and polynomial orders such that the number of degrees of freedom (DOFs) in the solution ranges from 50 to 410 million. Mean velocity results and root mean square (RMS) values of velocity fluctuations indicate a better agreement with experimental data as the resolution is increased. The generated data provide a good understanding of the effects of increasing the discretization refinement for LES calculations of jet flows. The present results can guide future simulations of similar flow configurations.

Fichier(s) constituant cette publication

Nom:
DYNFLUID_AIAAFORUM_2022_JUNQUE ...
Taille:
1.553Mo
Format:
PDF
Fin d'embargo:
2022-12-01
Voir/Ouvrir

Cette publication figure dans le(s) laboratoire(s) suivant(s)

  • Dynamique des Fluides (DynFluid)

Documents liés

Visualiser des documents liés par titre, auteur, créateur et sujet.

  • A comparison of low and high-order methods for the simulation of supersonic jet flows 
    Conférence invitée
    F. ABREU, Diego; T. V. DAURICIO, Eron; F. AZEVEDO, João Luiz; JUNQUEIRA-JUNIOR, Carlos (ABCM, 2021-11)
    The present work compares results for different numerical methods in search of alternatives to improve the quality of large-eddy simulations for the problem of a supersonic turbulent jet flows. Previous work has analyzed ...
  • External Laminar Boundary Layer Simulations Using a High-Fidelity Wall-Modeling Approach 
    Conférence invitée
    VIANA DAURICIO, Eron Tiago; ccJUNQUEIRA JUNIOR, Carlos; FEROLLA DE ABREU, Diego; AZEVEDO, João Luiz F. (ABCM, 2022-11)
    Wall-Modeled Large Eddy Simulation (WMLES) is a well-stablished technique for obtaining high-fidelity solutions of turbulent, high Reynolds number flows, with reasonably acceptable computational costs. However, for external ...
  • Large-eddy simulations of turbulent compressible supersonic jet flows using discontinuous Galerkin methods 
    Communication avec acte
    F. ABREU, Diego; ccJUNQUEIRA JUNIOR, Carlos; ccDAURICIO, Eron; F. AZEVEDO, João Luiz (Scipedia S.L., 2022-06)
    In this work, a discontinuous Galerkin scheme is employed to perform the simulations of supersonic jet flows. A total of four simulations are performed with different meshes and order of accuracy. The number of degrees of ...
  • On the scalability of CFD tool for supersonic jet flow configurations 
    Article dans une revue avec comité de lecture
    JUNQUEIRA-JUNIOR, Carlos; AZEVEDO, João Luiz F.; PANETTA, Jairo; WOLF, William R.; YAMOUNI, Sami (Elsevier, 2020)
    New regulations are imposing noise emissions limitations for the aviation industry which are pushing researchers and engineers to invest efforts in studying the aeroacoustics phenomena. Following this trend, an in-house ...
  • Strong scaling of numerical solver for supersonic jet flow configurations 
    Article dans une revue avec comité de lecture
    JUNQUEIRA-JUNIOR, Carlos; AZEVEDO, João Luiz F.; PANETTA, Jairo; WOLF, William R.; YAMOUNI, Sami (Springer Verlag, 2019)
    Acoustics loads are rocket design constraints which push researches and engineers to invest efforts in the aeroacoustics phenomena which is present on launch vehicles. Therefore, an in-house computational fluid dynamics ...

Parcourir

Tout SAMLaboratoiresAuteursDates de publicationCampus/InstitutsCe LaboratoireAuteursDates de publicationCampus/Instituts

Lettre Diffuser la Science

Dernière lettreVoir plus

Statistiques de consultation

Publications les plus consultéesStatistiques par paysAuteurs les plus consultés

ÉCOLE NATIONALE SUPERIEURE D'ARTS ET METIERS

  • Contact
  • Mentions légales

ÉCOLE NATIONALE SUPERIEURE D'ARTS ET METIERS

  • Contact
  • Mentions légales