Crossing regions for supersonic cones

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
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Acceso en línea:http://hdl.handle.net/11086/23227
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Sumario: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.