Passive flow modification over the supersonic and the hypersonic air-intake system using bleed

The air intake should be operated at design conditions to achieve a high total pressure recovery and optimum mass capture ratio. The current research focuses on the numerical simulation of the supersonic and hypersonic air inlet and its starting and unstarting characteristics. 2D RANS equation for s...

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Bibliographic Details

Published in:	FME Transactions
Main Authors:	Sinha Jayanta, Singh Sanjay, Prakash Om, Panchal Dhruv
Format:	Article
Language:	English
Published:	University of Belgrade - Faculty of Mechanical Engineering, Belgrade 2023-01-01
Subjects:	hypersonic inlet pressure recovery mass capture ratio shockwave starting and unstarting of inlet bleed geometry total pressure ratio
Online Access:	https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2023/1451-20922303329S.pdf