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Detailed Simulations of Shock-Bifurcation and Ignition of an Argon-diluted Hydrogen/Oxygen Mixture in a Shock Tube...

by Matthias Ihme, Yong Sun, Ralf Deiterding
Publication Type
Conference Paper
Book Title
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Publication Date
Conference Name
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Conference Location
Grapevine (Dallas/Ft. Worth Region), Texas, United States of America
Conference Sponsor
AIAA
Conference Date
-

Detailed simulations of the bifurcation and ignition of an Argon-diluted Hydrogen/Oxygen mixture in the two-stage weak ignition regime are performed. An adaptive mesh-refinement (AMR) technique is employed to resolve all relevant physical scales that are associated with the viscous boundary-layer, the reaction front, and the shock-wave. A high-order hybrid WENO/central-differencing method is used as spatial discretization scheme, and a detailed chemical mechanism is employed to describe the combustion of the H2/O2 mixture. The operating conditions considered in this study are p = 5 bar and T = 1100 K, and fall in the third explosion limit. The computations show that the mixing of the thermally stratified fluid, carrying different momentum and enthalpy, introduces inhomogeneities in the core-region behind the reflected shock. These inhomogeneities act as localized ignition kernels. During the induction period, these kernels slowly expand and eventually transition to a detonation wave that rapidly consumes the unburned mixture.In competition with this detonation wave are the presence of secondary ignition kernels that appear in the unreacted core-region between reflected shock and detonation wave.