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Analysis and modeling of bypass boundary layer transition

Grant number: 20/14200-5
Support type:Scholarships in Brazil - Doctorate (Direct)
Effective date (Start): June 01, 2021
Effective date (End): May 31, 2024
Field of knowledge:Engineering - Aerospace Engineering - Aerodynamics
Principal researcher:André Valdetaro Gomes Cavalieri
Grantee:Diego Chou Pazo Blanco
Home Institution: Pró-Reitoria de Pós-Graduação e Pesquisa. Instituto Tecnológico de Aeronáutica (ITA). Ministério da Defesa (Brasil). São José dos Campos , SP, Brazil

Abstract

The focus of the present study will be the application of the SPOD (Spectral Proper Orthogonal Decomposition) method and resolvent analysis in transitional flows over flat plates, not yet studied by this method, from spatio-temporal databases of simulations already existing in the laboratory. The aim will be to better characterize free turbulence transition (bypass) mechanisms not yet fully understood. With these same methods, the effects of the leading edge on the transition over flat plates will be studied. (AU)

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