The effects of bluntness and sweep on glancing shock wave turbulent boundary layer interaction
An experimental investigation has been performed into the effects of leading edge bluntness and sweep on the mean flow characteristics of a glancing shock wave turbulent boundary layer interaction. A series of blunt un swept shock generators (ranging in leading edge diameter from O to 1.0 ins) and a...
| Main Author: | |
|---|---|
| Other Authors: | |
| Published: |
Cranfield University
1986
|
| Subjects: | |
| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.685936 |