Authors: John R. Cipolla
A series of computational fluid dynamic (CFD) analysis and experiment is discussed that probes the interaction between multiple shock waves and the adjacent boundary layer at high supersonic speed. For a cone-cylinder-flare configuration the viscous boundary layer and its interaction with the outer flow field is computationally determined and then compared to an experimental technique using holographic interferometry. Ultimately, the base flow region of a projectile can be modeled using CFD and its results compared to experimental interferometric data during the validation stage of code development.
Comments: 9 Pages.
Download: PDF
[v1] 2015-04-23 14:37:58
[v2] 2024-03-06 14:02:20
[v3] 2024-03-19 13:53:31
Unique-IP document downloads: 174 times
Vixra.org is a pre-print repository rather than a journal. Articles hosted may not yet have been verified by peer-review and should be treated as preliminary. In particular, anything that appears to include financial or legal advice or proposed medical treatments should be treated with due caution. Vixra.org will not be responsible for any consequences of actions that result from any form of use of any documents on this website.
Add your own feedback and questions here:
You are equally welcome to be positive or negative about any paper but please be polite. If you are being critical you must mention at least one specific error, otherwise your comment will be deleted as unhelpful.