Characteristics of unsteady combustion around hypersonic cylindrical projectiles


A series of simulations were carried out to reproduce unsteady combustion around the hypervelocity cylindrical projectiles. A simplified two-step chemical reaction model was used to handle the reactions behind the bow shock. The simulations were examined with various parameters, such as projectile speed, initial pressure, and projectile diameter, and the… (More)


14 Figures and Tables

Slides referencing similar topics