The Effect of Oxidizer Particle Size Distribution on the Steady and Nonsteady Combustion of Composite Propellants.

摘要

A theoretical analysis of the combustion of composite propellants (with an emphasis on the heterogeneous effects) is presented. The analysis based on the combination of a unique statistical treatment of the burning surface with a very comprehensive multiple flame type of physiochemical model for the combustion process. The analysis is divided into four parts: the steady state burning rate, erosive burning rate, the pressure coupled response, and the velocity coupled response.