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Physics of Fluids
To further understand the muzzle combustion mechanism in high-altitude firing, the influence of supersonic flow on the muzzle combustion phenomenon is investigated. The set of internal ballistic equations is employed, providing accurate velocity and pressure when the projectile moves to the muzzle. The multispecies transport Navier-Stokes equations with complex chemical reactions is solved by coupling a real gas equation of state, the Soave-Redlich-Kwong Model, and a detailed chemical reactiondoi:10.1063/5.0131900 fatcat:tck6uhkkovdfnj6bznwyzw6ote