Chapman–Jouguet deflagration criteria and compressibility dynamics of turbulent fast flames for turbulence-induced deflagration-to-detonation transition

Author:

Chin Hardeo12ORCID,Chambers Jessica1,Poludnenko Alexei3ORCID,Gamezo Vadim N.4,Ahmed Kareem A.1ORCID

Affiliation:

1. Propulsion and Energy Research Laboratory, Center for Advanced Turbomachinery & Energy Research, Department of Mechanical and Aerospace Engineering, University of Central Florida 1 , Orlando, Florida 32816, USA

2. Lawrence Livermore National Laboratory, Physics Division, Applied Physics Group 2 , 7000 East Ave., Livermore, California 94550, USA

3. Department of Mechanical Engineering, University of Connecticut 3 , Storrs, Connecticut 06269 USA

4. Laboratories for Computational Physics and Fluid Dynamics, Naval Research Laboratory 4 , Washington, District of Columbia 20375, USA

Abstract

This work characterizes the compressibility dynamics in turbulent fast flames for a range of turbulent flame speeds. These turbulent fast flames experience increased effects of compressibility through the formation of strong shocks and may develop a runaway acceleration combined with a pressure buildup that leads to turbulence induced deflagration-to-detonation transition (tDDT). Simultaneous high-speed particle image velocimetry, OH* chemiluminescence, schlieren, and pressure measurements are used to examine the reacting flow field and flame dynamics. We examine flames with turbulent flame speeds ranging from 100 to 600 m/s. At lower turbulent flame speeds, the flame is not able to produce favorable background conditions for deflagration-to-detonation transition (DDT) onset, and thus flame compressibility and turbulence amplification are less dominant, resulting in a weaker acoustic coupling between the flame and compressed region. As the turbulent burning velocities exceed the Chapman–Jouguet deflagration speed, favorable background conditions are produced, as we observe flame-generated shocks and flame-generated turbulence with higher turbulent velocities and larger turbulent scales. At this regime, the flame is categorized to be at the runaway transition regime that leads to tDDT.

Funder

Air Force Office of Scientific Research

National Science Foundation

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Reference61 articles.

1. Detonation in gases;Proc. Combust. Inst.,2009

2. On the transition from deflagration to detonation,1992

3. Numerical simulation of deflagration-to-detonation transition: The role of shock–flame interactions in turbulent flames;Combust. Flame,1999

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