DIGITAL SIMULATION OF A HIGH-ENERGY SYSTEM USING A BORON–ALUMINUM ADMIXTURE AS A FUEL

Numerical modeling of the fl ow of combustion products of a fuel containing a boron–aluminum admixture in the nozzle of a solid-propellant rocket engine has been carried out. The advantage of boron–aluminum over aluminum in using in composite solid propellants has been shown.
   
Author:  N. N. D'yachenko and E. N. D'yachenko
Keywords:  two-phase fl ow, polydisperse ensemble of particles, two-phase loss, specifi c momentum
Page:  1347