On the influence of pressure variation on ignition and mixing processes in a reacting shock-bubble interaction

Conference paper (2015)

Authors

Felix Diegelmann Technische Universität München
Jan Matheis Technische Universität München
V. K. Tritschler Technische Universität München
S. Hickel Aerodynamics - Aerospace Engineering , Technische Universität München
Nikolaus A. Adams Technische Universität München
Research Group
Aerodynamics (Aerospace Engineering) (TU Delft)
More Info
expand_more

Published Date

01-01-2015

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Faculty

Aerospace Engineering

Department

Flow Physics and Technology

Research Group

Aerodynamics

Abstract

We present numerical simulations of a reacting shock-bubble interaction with detailed chemistry. The interaction of the Richtmyer-Meshkov instability (RMI) and shock-induced ignition of a stoichiometric H2-O2 gas mixture are investigated. Different initial pressures in the range of po = 0.25-0.75 atm at a constant shock wave Mach number of Ma = 2.30 trigger different reaction wave types (deflagration and detonation). Low pressure reactions are dominated by H, O, OH production and high pressure chemistry is driven by HO2 and H2O2. The reaction wave type is crucial for the spatial and temporal evolution of the bubble. The RMI and subsequent Kelvin Helmholtz instabilities show a high reaction sensitivity. Mixing is significantly reduced by both types of reaction waves, with detonation waves showing the strongest effect.