%0 Journal Article
%T CFD Analysis of Wall Injection with Large Sized Cavity Based Scramjet Combustion at Mach 2.
%A A. Rajkhowa
%A K Barman
%A K. M. Pandey
%A P Kalita
%A S. N. Saikia
%J International Journal of Engineering and Technology
%@ 1793-8236
%D 2011
%R 10.7763/IJET.2011.V3.210
%X Abstract¡ªA CFD analysis of the combustion process of a scramjet engine having wall injector with cavity with a L/Dratio of 5 is carried out in this present study using FLUENT software. Both air intake and H2 injection are at Mach 2 speed and hydrogen is being injected upstream of the cavity. It is observed that a maximum temperature of 2100K can be achieved with the injection of H2 at Mach 2 speed with high thrust production and low shock formation.
%U http://www.ijetch.org/show-36-163-1.html