The numerical solution of certain differential equations occurring in Crocco's theory of the laminar boundary layer
Loading...
Date published
Free to read from
Authors
Supervisor/s
Industry supervisor/s
Journal Title
Journal ISSN
Volume Title
Publisher
Department
Course name
Type
ISSN
Format
Citation
Abstract
A numerical method is described for the solution of certain differential equations which result from the application of Crocco’s transformation to the laminar boundary layer equations appropriate to high supersonic Mach numbers. (i.e. at hypersonic speeds). Continues …