4.0 Article Proceedings Paper

The use of OH* and CH* as heat release markers in combustion dynamics

Journal

Publisher

SAGE PUBLICATIONS INC
DOI: 10.1177/1756827717718483

Keywords

Chemiluminescence; rocket combustion instability; time accurate Computational Fluid Dynamics (CFD); detailed kinetics

Funding

  1. Air-Force Office of Scientific Research

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The study examines chemiluminescence measurements and computations as a method of validation. Because chemiluminescent radicals are present in small concentrations and associated timescales are also small, a common assumption is that these are quasi-steady-state species and their transport can be ignored. This paper examines the above assumption using available data and simulation results, specifically aiming at a single element rocket combustor under strong pressure fluctuations. Variations in the kinetics rate constants are considered for assessing sensitivity of the results. Two additional aspects are explored: the ability of the excited species to represent the chemical heat release and the optical thickness of the medium. For the conditions of the study, the quasi-steady-state assumption in the case of OH* is found to be marginally insufficient while in the case of CH*, it is found to be acceptable. Modeled heat release is qualitatively better captured by CH* than OH* because of higher difference in the peak to asymptotic concentrations and lower ground state concentration.

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