Experimental study of high-speed air intake performance by side clearance
S Ogura, M Fujii, Y Hoshiya, Y Fujimori, T Sato… - Aerospace Science and …, 2022 - Elsevier
Abstract Japan Aerospace Exploration Agency (JAXA) and universities plan the “High Mach
Integrated Control Experiment”(HIMICO), which is a hypersonic flight test by JAXA's S-520 …
Integrated Control Experiment”(HIMICO), which is a hypersonic flight test by JAXA's S-520 …
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 …
carried out with and without air jets (AJs) at design Mach number of 2.2. Reynolds-averaged …
The study of cascading effect in the integration of intake with gas turbine engine bay in subsonic cruise vehicle
TV Yogesh, LP Nidamarty… - International Journal of …, 2024 - degruyter.com
Submerged air intake is often acquainted with the merit of reducing the drag and fitting well
within the frame of weight constraints imposed on subsonic cruise vehicle. A novel method …
within the frame of weight constraints imposed on subsonic cruise vehicle. A novel method …
Mitigating Shock Wave Challenges through Extended Bleed Technique in Mixed Compression Supersonic Air Intake
S Jogu, K Das - 2024 Regional Student Conferences, 2024 - arc.aiaa.org
This study delves into enhancing the performance of supersonic air intakes by addressing
shock wave-related challenges through the implementation of secondary recirculation …
shock wave-related challenges through the implementation of secondary recirculation …
Effect of Turbulence Modeling on the Performance of Mixed Compression Supersonic Air Intake
NK SINGH - essopenarchive.org
The purpose of this study is to assess the effect of turbulence modeling on the flow field and
on the performance of supersonic air intake at designed Mach number. Various turbulence …
on the performance of supersonic air intake at designed Mach number. Various turbulence …