ABSTRACT

A two phase base bleed base combustion model has been presented in which the exit area ratio, jet solid-phase particle mass ratio, fuel enthalpy of combustion, molecular weight of the gas, stagnation temperature in the chamber, flight Mach number parameters have been considered. In the present paper, a practical calculating method has been given completely, and varied estimation examples have been taken. The comparison of these results with many available experimental data shows generally good agreement.