Aerodynamic assessment of axisymmetric launchers in the context of multidisciplinary optimisation

The paper presents a fast mathematical model that can be used to quickly assess the aerodynamic force coefficients of axisymmetric launchers as functions of Mach number and angle of attack. The tool developed based on the proposed mathematical model can be used separately or it can be integrated in...

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Detalhes bibliográficos
Main Authors: Alexandru-Iulian ONEL, Teodor-Viorel CHELARU
Formato: Artigo
Idioma:Inglês
Publicado em: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2020-03-01
Colecção:INCAS Bulletin
Assuntos:
mathematical model
aerodynamic force coefficients
axisymmetric launcher
multidisciplinary optimisation
Acesso em linha:http://bulletin.incas.ro/files/onel__chelaru__vol_12_iss_1.pdf
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