Wind tunnel wall boundary layer control for 2D high lift wing testing (2004)
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
ABNT
CATALANO, Fernando Martini e CAIXETA JUNIOR, Paulo Roberto. Wind tunnel wall boundary layer control for 2D high lift wing testing. 2004, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2004. . Acesso em: 03 out. 2024.APA
Catalano, F. M., & Caixeta Junior, P. R. (2004). Wind tunnel wall boundary layer control for 2D high lift wing testing. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.NLM
Catalano FM, Caixeta Junior PR. Wind tunnel wall boundary layer control for 2D high lift wing testing. Proceedings. 2004 ;[citado 2024 out. 03 ]Vancouver
Catalano FM, Caixeta Junior PR. Wind tunnel wall boundary layer control for 2D high lift wing testing. Proceedings. 2004 ;[citado 2024 out. 03 ]