Result: Numerical simulations of transonic aerodynamic flows based on a hierarchical formulation
Title:
Numerical simulations of transonic aerodynamic flows based on a hierarchical formulation
Authors:
Source:
Advances and challenges in flow simulation and modelling: minisymposium at the 5th World Congress on Computational Mechanics, July 7-12, 2002, Vienna, AustriaInternational journal for numerical methods in fluids. 47(6-7):491-516
Publisher Information:
Chichester: Wiley, 2005.
Publication Year:
2005
Physical Description:
print, 34 ref
Original Material:
INIST-CNRS
Subject Terms:
Mechanics acoustics, Mécanique et acoustique, Sciences exactes et technologie, Exact sciences and technology, Physique, Physics, Domaines classiques de la physique (y compris les applications), Fundamental areas of phenomenology (including applications), Mécanique des fluides, Fluid dynamics, Méthodes de calcul en mécanique des fluides, Computational methods in fluid dynamics, Mécanique des fluides appliquée, Applied fluid mechanics, Aérodynamique, Aerodynamics, Aérodynamique, Aerodynamics, Distribution pression, Pressure distribution, Distribución presión, Distribution vitesse, Velocity distribution, Ecoulement transsonique, Transonic flow, Interaction visqueuse non visqueuse, Viscous non viscous interaction, Interacción viscosa no viscosa, Mécanique fluide numérique, Computational fluid dynamics, Simulation numérique, Digital simulation, Système hiérarchisé, Hierarchical systems, Helmholtz decomposition, viscous and inviscid transonic flows
Document Type:
Conference
Conference Paper
File Description:
text
Language:
English
Author Affiliations:
University of California, Duvis CA 95646, United States
ISSN:
0271-2091
Rights:
Copyright 2005 INIST-CNRS
CC BY 4.0
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
CC BY 4.0
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
Notes:
Physics: fluid mechanics
Accession Number:
edscal.16594196
Database:
PASCAL Archive
Further Information
Steady two-dimensional potential flows over airfoils are calculated with and without entropy and vorticity corrections, due to the presence of shock waves and/or laminar boundary layers.