Numerical study of oblique detonation initiations with chain branching kinetics

Honghui Teng, Pengfei Yang, Zonglin Jiang

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

6 Citations (Scopus)

Abstract

Oblique detonations induced by semi-infinite wedge are simulated by solving Euler equations with chain branching kinetics. Numerical results show the initiation can be triggered by either the abrupt transition or smooth transition, dependent on incident Ma Min and wedge angle θ, and then their effects on the oblique detonation angle β and initiation length Lini are analyzed. When θ increases, Lini decreases monotonically but β has a minimum value, corresponding to θ = 29° in this study. When Min decreases, both Lini and β increases monotonically until Min decreases below certain critical value, Min = 9.2 in this study. Then low inflow Ma effects generate the maximum Lini, with the complex of ODW (oblique detonation wave), SODW (secondary oblique detonation wave) and SIDW (self-ignition deflagration wave). The transient process is observed, demonstrating the structure can self-adjust to find a proper position. The wave structure suggests two wave/heat release process determining the detonation initiation. In the cases with high Min featured by SIDW, the oblique-shock induced self-ignition dominates, and Lini increases when Min decreases. In the cases with low Min featured by SODW, the interaction of ODW and SODW dominates, and Lini decreases when Min decreases.

Original languageEnglish
Title of host publicationAIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Electronic)9781624104473
DOIs
Publication statusPublished - 2017
Externally publishedYes
Event55th AIAA Aerospace Sciences Meeting - Grapevine, United States
Duration: 9 Jan 201713 Jan 2017

Publication series

NameAIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting

Conference

Conference55th AIAA Aerospace Sciences Meeting
Country/TerritoryUnited States
CityGrapevine
Period9/01/1713/01/17

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