Numerical study of supersonic mixed compression air intake with an array of air jets

NK Gahlot, NK Singh - Journal of Fluids Engineering, 2021 - asmedigitalcollection.asme.org
Computational study of flow physics inside the mixed compression air intake has been
carried out with and without air jets (AJs) at design Mach number of 2.2. Reynolds-averaged …

Performance Study of Supersonic Air-intake Adopting Double Bump

MM Dhanlobhe, PD Nale, VS Shejwal… - 2021 IEEE Pune …, 2021 - ieeexplore.ieee.org
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 …

[PDF][PDF] Comparative Analysis of External Supersonic Air Inlet Shocks

J Nagler - researchgate.net
This study uses numerical methods to analyze the design of air intake components for
Ramjet and Scramjet engines. It focuses on the external geometry of the intake, including …