Abstract
The effects of material interface curvature on deflagration of a homogeneous solid energetic material (EM) is studied in a limit when the radius of curvature is much larger than the deflagration front thickness. Under the assumption of quasi-steady burning, a method of matched asymptotics is employed do derive first-order curvature corrections to the mass flux across the gas-solid interface as well as to the interface temperature. As an illustration, a problem of quasi-steady spherical particle deflagration is solved numerically and the simulation results are used to verify those obtained through asymptotic analysis. An algorithm for a fully-coupled unsteady solver suitable for EM deflagration simulation is presented. Numerical solution of the unsteady spherical particle deflagration is used to show that the assumption of quasi-steady deflagration is valid.
Original language | English (US) |
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Pages (from-to) | 615-637 |
Number of pages | 23 |
Journal | Combustion Theory and Modelling |
Volume | 11 |
Issue number | 4 |
DOIs | |
State | Published - Aug 2007 |
Keywords
- Asymptotic
- Curvature
- Deflagration
- Particle
- Propellant
ASJC Scopus subject areas
- General Chemistry
- General Chemical Engineering
- Modeling and Simulation
- Fuel Technology
- Energy Engineering and Power Technology
- General Physics and Astronomy