Shock boundary layer interaction structure
Journal
International Journal of Turbo and Jet Engines
Journal Volume
14
Journal Issue
4
Pages
229-238
Date Issued
1997
Author(s)
Sheu, T.W.H.
Abstract
A model is presented to study the interaction between an oblique shock and a fully-unseparated turbulent boundary layer over the nonadiabatic wall. The method of matched asymptotic expansion, valid in the double limit of free-stream.
SDGs
Type
journal article