Strong scaling of numerical solver for supersonic jet flow configurations

Strong scaling of numerical solver for supersonic jet flow configurations

Carlos Junqueira-Junior, Joao Luiz F. Azevedo, Jairo Panetta, William R. Wolf, Sami Yamouni

ARTIGO

Inglês

Acoustics loads are rocket design constraints which push researches and engineers to invest efforts in the aeroacoustics phenomena which is present on launch vehicles. Therefore, an in-house computational fluid dynamics tool is developed in order to reproduce high-fidelity results of supersonic jet...

CONSELHO NACIONAL DE DESENVOLVIMENTO CIENTÍFICO E TECNOLÓGICO - CNPQ

FUNDAÇÃO DE AMPARO À PESQUISA DO ESTADO DE SÃO PAULO - FAPESP

Fechado

Strong scaling of numerical solver for supersonic jet flow configurations

Carlos Junqueira-Junior, Joao Luiz F. Azevedo, Jairo Panetta, William R. Wolf, Sami Yamouni


										

Strong scaling of numerical solver for supersonic jet flow configurations

Carlos Junqueira-Junior, Joao Luiz F. Azevedo, Jairo Panetta, William R. Wolf, Sami Yamouni

    Fontes

    Journal of the Brazilian Society of Mechanical Sciences and Engineering

    Vol. 41, no. 12 (Dec., 2019), n. art. 547