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.
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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|
|Depositing User:||epEditor USQ|
|Date Deposited:||30 Oct 2011 08:43|
|Last Modified:||03 Jul 2013 00:46|
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