Numerical modeling of auto-ignition of isolated fuel droplets in microgravity

Abstract In this work we present and apply a mathematical model to simulate the auto-ignition of isolated fuel droplets burning in microgravity conditions. The aim is to demonstrate the fundamental role of the low-temperature mechanisms on the auto-ignition process and to show that several experimental observations cannot be explained without considering the formation of cool-flames around the burning droplet. Thus, in order to better clarify the importance of the low-temperature chemistry, a detailed kinetic scheme (with hundreds of species and thousands of reactions) was adopted to model the spontaneous ignition of isolated droplets of n -heptane, n -decane, and n -dodecane in air, in a wide range of operating conditions (with environment temperatures from 600 K to 1100 K and pressures from 1 bar to 20 bar). The model was able to correctly identify the typical auto-ignition regimes of n -alkane oxidation. The comparison with the experimental measurements available in the literature was satisfactory: both first-stage and total induction times were reasonably captured by the numerical simulations. The simulations confirmed that the low-temperature chemistry plays a role of paramount importance in the auto-ignition process. In particular, the competition between low- and high-temperature mechanisms was found to explain the different types of auto-ignition which can be experimentally observed.

[1]  Jordan Conley,et al.  Detailed modeling of an isolated, ethanol droplet combustion under microgravity conditions , 2003 .

[2]  C. Law,et al.  Hierarchical and comparative kinetic modeling of laminar flame speeds of hydrocarbon and oxygenated fuels , 2012 .

[3]  T. E. Daubert,et al.  Data compilation tables of properties of pure compounds , 1985 .

[4]  A. Marchese,et al.  The effect of liquid mass transport on the combustion and extinction of bicomponent droplets of methanol and water , 1996 .

[5]  F. Dryer,et al.  Isolated n-heptane droplet combustion in microgravity: “Cool Flames” – Two-stage combustion , 2014 .

[6]  M. Frenklach,et al.  Transport properties of polycyclic aromatic hydrocarbons for flame modeling , 1994 .

[7]  Davide Manca,et al.  BzzOde: a new C++ class for the solution of stiff and non-stiff ordinary differential equation systems , 1998 .

[8]  A. Marchese,et al.  Microgravity n-Heptane Droplet Combustion in Oxygen-Helium Mixtures at Atmospheric Pressure , 1998 .

[9]  Christian Eigenbrod,et al.  Effects of dilution by aromatic hydrocarbons on staged ignition behavior of n-decane droplets , 2000 .

[10]  C. Eigenbrod,et al.  Detailed numerical simulations for the multi-stage self-ignition process of n-decane single droplets with complex chemistry , 2001 .

[11]  S. Sazhin Advanced models of fuel droplet heating and evaporation , 2006 .

[12]  C. Eigenbrod,et al.  Numerical analysis of the cool flame behavior of igniting n-Heptane droplets , 2005 .

[13]  M. Mehl,et al.  Autoignition and burning rates of fuel droplets under microgravity , 2005 .

[14]  Osamu Moriue,et al.  DETAILED NUMERICAL SIMULATIONS OF THE MULTISTAGE SELF- IGNITION PROCESS OF n-HEPTANE ISOLATED DROPLETS AND THEIR VERIFICATION BY COMPARISON WITH MICROGRAVITY EXPERIMENTS , 2000 .

[15]  E. Ranzi,et al.  Lumping and Reduction of Detailed Kinetic Schemes: an Effective Coupling , 2014 .

[16]  Peter M. Struk,et al.  Inverse influence of initial diameter on droplet burning rate in cold and hot ambiences: a thermal action of flame in balance with heat loss , 2003 .