Theoretical investigation of shock stand-off distance for non-equilibrium flows over spheres
KAUST DepartmentComputer, Electrical and Mathematical Sciences and Engineering (CEMSE) Division
Extreme Computing Research Center
Online Publication Date2018-02-20
Print Publication Date2018-05
Permanent link to this recordhttp://hdl.handle.net/10754/627185
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AbstractWe derived a theoretical solution of the shock stand-off distance for a non-equilibrium flow over spheres based on Wen and Hornung’s solution and Olivier’s solution. Compared with previous approaches, the main advantage of the present approach is allowing an analytic solution without involving any semi-empirical parameter for the whole non-equilibrium flow regimes. The effects of some important physical quantities therefore can be fully revealed via the analytic solution. By combining the current solution with Ideal Dissociating Gas (IDG) model, we investigate the effects of free stream kinetic energy and free stream dissociation level (which can be very different between different facilities) on the shock stand-off distance.
CitationSHEN H, WEN C-Y (2018) Theoretical investigation of shock stand-off distance for non-equilibrium flows over spheres. Chinese Journal of Aeronautics. Available: http://dx.doi.org/10.1016/j.cja.2018.02.013.
SponsorsThis study was co-supported by the Research Grants Council of Hong Kong, China (No. C5010-14E) and the National Natural Science Foundation of China (No. 11372265).
JournalChinese Journal of Aeronautics
Except where otherwise noted, this item's license is described as © 2018. This manuscript version is made available under the CC-BY-NC-ND 4.0 license http://creativecommons.org/licenses/by-nc-nd/4.0/