Laminariscent Turbulent Boundary Layers
Auteur : Roger L. Simpson, C. R. Shackleton
Date de publication : 1977
Éditeur : Defense Technical Information Center
Nombre de pages : 107
Résumé du livre
Because a turbulent boundary layer in a nozzle undergoes strong acceleration, a laminariscent boundary layer with the benefit of a lower surface heat transfer rate can result for some short distance. Here several phenomena which accompany laminarescence produced by strong acceleration are examined for nozzle-flow and sink-flow accelerational distributions, respectively.