Aerospace Engineering Colloquium, Meredith B. Colket- Selected Cool Flame Phenomena

Friday, December 8, 2023
3:00 p.m.
Location

United States

Floor/Room #
2nd floor/ Room #229

Graduate Colloquium, Aerospace Engineering Presents Meredith B. Colket, and the Selected Cool Flame Phenomena 

Significant research associated with cool flames and transitions to hotter flames for large molecular weight alkane fuels has been performed. Much of this prior work reports ignition delay times for cool flames and then for transition to hot flames as a function of various parameters and describes development of detailed reaction mechanisms that simulate such phenomena. This paper addresses two aspects of cool flames that have received less focus: (Q1) why does a cool flame stop burning, even though sufficient reactants remain unburned, and (Q2) can an equivalence ratio of a cool flame be defined, given that the ratio of the oxidizer to original fuel consumed in the cool flame varies significantly from the starting ratios of their concentrations? To examine these questions, we use simulation results from a detailed chemical kinetic model for combustion of nondecane over a range of conditions. Where possible, we also examine recent experimental data sets for comparisons to our conclusions. In the case of Q1, we consider three possibilities: A. Chemical heat release pushing reactions into the slower NTC region (traditional explanation for termination of cool flames), B. Depletion of the parent fuel leading to slower overall reaction rates. And C. Supply of hydro-peroxide and other high MW product species produced during induction and/or in the flame becomes exhausted, shutting down the chain branching processes. Each phenomenon is considered and assessed for their role in the termination of the cool flame reactivity. In addition, the relative consumption of O2 vs. n-dodecane is tracked and compared over a variety of conditions, as well as typical product distributions resulting from the cool flame reactions. Comparisons to high temperature ignition phenomena for (high MW) hydrocarbon fuels in which the parent fuel pyrolyzes to a set of product species that govern subsequent ignition times are considered.

Audience(s)

Department(s):

Aerospace Engineering
Contact Person
Joanne Tripp

Phone Number:

ATTACHMENT