Effects of non-thermal termolecular reactions on wedge-induced oblique detonation waves

The shock-induced combustion ramjet (Shcramjet) based on oblique detonation waves (ODWs) is among the promising choices for hypersonic propulsion systems. An understanding of the ignition, propagation, and stability of ODWs is critical to harnessing their propulsive potential. In such high speed rea...

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Veröffentlicht in:	Combustion and flame 2023-03, Vol.257
Hauptverfasser:	Desai, Swapnil, Tao, Yujie, Sivaramakrishnan, Raghu, Chen, Jacqueline H.
Format:	Artikel
Sprache:	eng
Schlagworte:	chemically reacting flows computational fluid dynamics simulations hypersonic propulsion kinetics nonequilibrium nonequilibrium kinetics oblique detonation termolecular reactions
Online-Zugang:	Volltext
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