Investigation Of Boundary Layer Transition In Three-Dimensional Supersonic Flow Over Sharp Cone
Abstract
Investigations of boundary layer transition on sharp cone surface are presented. The dependence is found for transition front configuration on the cone surface against relative angle of attack and general similarity parameters of viscous supersonic flows. The influence of boundary layer state variation on cone aerodynamic characteristics is analysed for three-dimensional flows.
- Publication:
-
7th European Symposium on Aerothermodynamics
- Pub Date:
- May 2011
- Bibcode:
- 2011ESASP.692E..82K