Further development of a hybrid particle-continuum method for transitional hypersonic flows

【Author】

Ashley M.Verhoff;Iain D.Boyd;

【Abstract】

<正>Hypersonic re-entry vehicles encounter a range of flight regimes,from rarefied conditions in the upper atmosphere to fully continuum at low altitudes.At transitional Knudsen numbers,there are likely to be localized regions of thermodynamic nonequilibrium effects for which the assumptions of the Navier–Stokes equations are no longer applicable.Because of the mixed rarefied-continuum nature of these types of flows,there is much to be gained in terms

【Keywords】

DSMC;Further development of a hybrid particle-continuum method for transitional hypersonic flows;MPC;

References

To explore the background and basis of the node document

Springer Journals Database

Total: 2 articles

  • [1] T.E. Schwartzentruber;;L.C. Scalabrin;;I.D. Boyd, A modular particle–continuum numerical method for hypersonic non-equilibrium gas flows, Journal of Computational Physics,
  • [2] Verhoff A M;Boyd I D, Consistent modeling of rotational nonequilibrium in a hybrid particlecontinuum method, AIAA Paper 2013 -3145,

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