Supersonic flow past an airfoil

Fuente: arXiv
Enregistré dans:
Détails bibliographiques
Auteur principal: Angelopoulos, Yannis
Format: Preprint
Publié: 2023
Sujets:
Accès en ligne:
Tags: Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!
_version_ 1866929197229801472
author Angelopoulos, Yannis
author_facet Angelopoulos, Yannis
contents We consider a supersonic flow past an airfoil in the context of the steady, isentropic and irrotational compressible Euler equations. We show that for appropriate data, either a shock forms, in which case certain derivatives of the solution blow up, or a sonic line forms, which translates to the fact that the hyperbolic character of the equations degenerates.
format Preprint
id arxiv_https___arxiv_org_abs_2312_17408
institution arXiv
publishDate 2023
record_format arxiv
spellingShingle Supersonic flow past an airfoil
Angelopoulos, Yannis
Analysis of PDEs
We consider a supersonic flow past an airfoil in the context of the steady, isentropic and irrotational compressible Euler equations. We show that for appropriate data, either a shock forms, in which case certain derivatives of the solution blow up, or a sonic line forms, which translates to the fact that the hyperbolic character of the equations degenerates.
title Supersonic flow past an airfoil
topic Analysis of PDEs
url https://arxiv.org/abs/2312.17408