Numerical analyses of a reference wing for combination of hybrid laminar flow control and variable camber

The objective of the LuFo VI-1 project CATeW (Coupled Aerodynamic Technologies for Aircraft Wings) consists in multifidelity analyses to assess the potential for aerodynamic efficiency increase by combined application of hybrid laminar flow control and variable camber technologies to the wing of a t...

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Detalles Bibliográficos
Autores principales: Jentys, Mauricio M., Effing, Tim, Breitsamter, Christian, Stumpf, Eike
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Springer Vienna 2022
Materias:
Original Paper
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9294800/
https://www.ncbi.nlm.nih.gov/pubmed/35874442
http://dx.doi.org/10.1007/s13272-022-00598-y

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9294800/
https://www.ncbi.nlm.nih.gov/pubmed/35874442
http://dx.doi.org/10.1007/s13272-022-00598-y

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