Numerical simulations of oblique detonations in supersonic combustion chambers

The concept of oblique detonation waves has been suggested as an efficient mechanism for ignition of the combustible mixture in a scramjet. To verify this concept, both experimental and numerical capabilities must be developed. The authors have developed an inviscid, two-dimensional numerical scheme...

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Veröffentlicht in:	Journal of propulsion and power 1989-07, Vol.5 (4), p.482-491
Hauptverfasser:	Cambier, Jean-Luc, Adelman, Henry G, Menees, Gene P
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft Propulsion And Power Combustion chambers Computer simulation ignition shock waves Supersonic combustion
Online-Zugang:	Volltext
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