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Analysis and modeling of bypass boundary layer transition

Grant number: 19/19000-7
Support Opportunities:Scholarships in Brazil - Master
Effective date (Start): December 01, 2019
Effective date (End): May 31, 2021
Field of knowledge:Engineering - Aerospace Engineering - Aerodynamics
Principal Investigator:André Valdetaro Gomes Cavalieri
Grantee:Diego Chou Pazo Blanco
Host 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. (AU)

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