Blunt body rarefied wakes for Earth entry

Direct simulation Monte Carlo (DSMC) and Navier-Stokes axisymmetric calculations are presented for hypersonic low-density flow about a 70-deg blunt cone afterbody configuration. The flow conditions simulated are those experienced by a space vehicle for an altitude range of 105-75 km during Earth ent...

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Bibliographische Detailangaben

Veröffentlicht in:	Journal of thermophysics and heat transfer 1995-07, Vol.9 (3), p.464-470
Hauptverfasser:	Dogra, Virendra K, Moss, James N, Wilmoth, Richard G, Taylor, Jeff C, Hassan, H. A
Format:	Artikel
Sprache:	eng
Schlagworte:	Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Jets Physics Rarefied gas dynamics Turbulent flows, convection, and heat transfer Wakes
Online-Zugang:	Volltext
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