...Mehdi Mohamadi; AmirMahdi Tahsini Purpose The purpose of this study is to investigate the combustion of the n-Heptane droplets in the supersonic combustor with a cavity-based fuel injection configuration. The focus is on the impacts of the droplet size on combustion efficiency. Design...

...Sathish Kumar K; Naren Shankar R; Anusindhiya K; Senthil Kumar B.R. Purpose This study aims to present the numerical study on supersonic jet mixing characteristics of the co-flow jet by varying lip thickness (LT). The LT chosen for the study is 2 mm, 7.75 mm and 15 mm. Design/methodology...

...AmirMahdi Tahsini Purpose The purpose of this paper is to analyze the effect of pressure fluctuations on the combustion efficiency of the hydrogen fuel injected into the supersonic oxidizing cross flow. The pressure fluctuations are imposed on inlet air flow and also on the fuel flow stream. Two...

... of jets by the usage of tabs of different geometries as vortex generators. Arun Kumar and Rathakrishnan (2014) presented the effectiveness of tabs that sheds small-scale vortices, which enhances the mixing at Mach 2 supersonic jet. Different geometries of corrugation (semi-circular, triangular...