Work

Analyses of Reynolds and Mach number effects on Tollmien–Schlichting wave–bump interaction in subsonic flows

Year: 2024

Type: article

Source: Journal of Fluid Mechanics

DOI: 10.1017/jfm.2024.675

Authors: Fernando H.T. Himeno, A.E.B. Carvalho, M.A.F. Medeiros

Institution: Universidade de São Paulo

Language: English

Topic: Fluid Dynamics and Turbulent Flows

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funders: Boeing, Fundação de Amparo à Pesquisa do Estado de São Paulo, Coordenação de Aperfeiçoamento de Pessoal de Nível Superior, Conselho Nacional de Desenvolvimento Científico e Tecnológico, Air Force Office of Scientific Research

Awards: G121811674, G2136218321, G2655881512, G3236259927, G4669957689, Experimental study of the effect of a cavity on boundary layer transition, G713732004, G8013126407, G850024020

OpenAlex ID: W4403773776

FWCI: 1.205

Cites: 48

Cited by: 6

Related to: 10