Morgan, R. G. and McIntyre, T. J. and Buttsworth, D. R. and Jacobs, P. A. and Potter, D. F. and Brandis, A. M. and Gollan, R. J. and Jacobs, C. M. and Capra, B. R. and McGilvray, M. and Eichmann, T. N. (2008) Impulse facilities for the simulation of hypersonic radiating flows. In: 38th AIAA Fluid Dynamics Conference and Exhibit (AIAA 2008), 23-26 Jun 2008, Seattle, WA. United States.
Metadata
| HTML Citation | EndNote | MODS | Dublin Core | Reference Manager |
Full text available as:
![[img]](/style/images/fileicons/application_pdf.png) | PDF (Published Version) - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader 975Kb |
Abstract
At high flight speeds, radiation becomes an important component of aerodynamic heat transfer, and its coupling with the flow field can significantly change macroscopic features of the flow. As radiating flight conditions are typically encountered in reentry trajectories, the associated flight regimes range from rarefied to continuum, and may have many levels of thermal, chemical and electronic non-equilibrium.
| Item Type: | Conference or Workshop Item (Commonwealth Reporting Category E) (Paper) |
|---|---|
| Additional Information: | Access to published version due to publisher copyright policy. (Form B at http://www.aiaa.org/pdf/home/authorkit.pdf) |
| Uncontrolled Keywords: | hypervelocity; aerodynamics; hypersonic; reentry |
| Fields of Research (FOR2008): | 09 Engineering > 0915 Interdisciplinary Engineering > 091508 Turbulent Flows 09 Engineering > 0915 Interdisciplinary Engineering > 091501 Computational Fluid Dynamics 09 Engineering > 0901 Aerospace Engineering > 090107 Hypersonic Propulsion and Hypersonic Aerodynamics |
| Subjects: | UNSPECIFIED |
| Socio-Economic Objective (SEO2008): | E Expanding Knowledge > 97 Expanding Knowledge > 970109 Expanding Knowledge in Engineering |
| ID Code: | 19605 |
| Deposited By: | |
| Deposited On: | 30 Oct 2011 18:43 |
| Last Modified: | 22 Dec 2011 09:39 |
Archive Staff Only: edit this record