Author : Oveepsa Chakraborty, Deepak Sharma, K. Obula Reddy, K. M Pandey [ Volume No. : I Issue No. : III - Nov. 2012] [Page No : 126-133] [2012]

This work involves an application of computational fluid dynamics to a problem associated with the flow in the combustor region of a supersonic combustion ramjet engine (Scramjet). The CFD analysis of the combustion process of a scramjet engine having wall injector at different position on the wall of the combustion nozzle with single cavity and double cavity for L/D ratio 10. The main objective of this work is to design the combustion chamber model by using GAMBIT software...