Numerical Simulation of JP 10 Combustion in Jet Engine for Missile
A customary numerical method was presently used to simulate the combustion of JP 10 in the turbojet for one missile.The result is compared with the RP 3's,which showed that,keeping the air inlet conditions same,JP 10 could combust normally.The region of flame with high temperature reduced and the heat loaded on the chamber descends after substituting JP 10 for RP 3.When keep the fuel mass flow rate same with the RP 3's,fuel supplying time increased about 20%,and the excite momentum and total temperature decreased about 3%.The non unity of the temperature distribution on the exit of the chamber and the heat loading on the turbine were reduced under the condition with the same fuel flux.