Crossing regions for supersonic cones

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The original study of a conical body of circular cross section at zero angle of attack inside a supersonic flow was developed by Taylor & Maccoll 1933, see [1]. After this year a large amount of numerical and perturbation techniques were developed to approximate solutions and to deal with the pr...

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Detalles Bibliográficos
Autores principales: Ferreyra, R. T., Tamagno, J. P.
Formato: conferenceObject
Lenguaje:Inglés
Publicado: 2022
Materias:
Shock waves
Copressible flow
Acceso en línea:http://hdl.handle.net/11086/23227
Aporte de:
Repositorio Digital Universitario (UNC) de Universidad Nacional de Córdoba
id I10-R14111086-23227
record_format dspace
institution Universidad Nacional de Córdoba
institution_str I-10
repository_str R-141
collection Repositorio Digital Universitario (UNC)
language Inglés
topic Shock waves
Copressible flow
spellingShingle Shock waves
Copressible flow
Ferreyra, R. T.
Tamagno, J. P.
Crossing regions for supersonic cones
topic_facet Shock waves
Copressible flow
description The original study of a conical body of circular cross section at zero angle of attack inside a supersonic flow was developed by Taylor & Maccoll 1933, see [1]. After this year a large amount of numerical and perturbation techniques were developed to approximate solutions and to deal with the problem.
format conferenceObject
author Ferreyra, R. T.
Tamagno, J. P.
author_facet Ferreyra, R. T.
Tamagno, J. P.
author_sort Ferreyra, R. T.
title Crossing regions for supersonic cones
title_short Crossing regions for supersonic cones
title_full Crossing regions for supersonic cones
title_fullStr Crossing regions for supersonic cones
title_full_unstemmed Crossing regions for supersonic cones
title_sort crossing regions for supersonic cones
publishDate 2022
url http://hdl.handle.net/11086/23227
work_keys_str_mv AT ferreyrart crossingregionsforsupersoniccones
AT tamagnojp crossingregionsforsupersoniccones
bdutipo_str Repositorios
_version_ 1764820396024004609

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