Mayuri M Dhanlobhe, Pritee D Nale, Vishal S Shejwal, Pratik A. Suryawanshi, D. Sahoo
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Performance Study of Supersonic Air-intake Adopting Double Bump
A computational study is carried out by adopting Two-Dimensional Double Bump at supersonic air intake for Mach number 2.2. Numerical simulation has been made with an Explicit coupled solver with K-ω turbulence model. The improvement in flow and overall performance of supersonic intake is observed with adoption of Double Bump. It has been observed that the pressure recovery is increased by installing Double Bump. Computational study revealed that the low-energy air region near the wall boundary layer has minimized for the case of double bump compared with that of the single bump air-intake.
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