Shock Structure Solution by Hybrid Flowfield Methods

A hybrid kinetic-based code, the Unified Flow Solver, is called on to investigate the internal structure of a normal shock wave for a Mach range of 1.55 to 9.0 for Argon, and 1.53 to 3.8 for diatomic Nitrogen. Reciprocal shock thickness, density, temperature, heat flux, and the partially-integrated...

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Veröffentlicht in:	Journal of spacecraft and rockets 2012-11, Vol.49 (6), p.1058-1068
Hauptverfasser:	Bentley, Brook I, Greendyke, Robert B
Format:	Artikel
Sprache:	eng
Schlagworte:	Argon Computer simulation Density Mathematical models Monte Carlo methods Navier-Stokes equations Shock waves Solvers
Online-Zugang:	Volltext
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