The Implication of Injection Locations in an Axisymmetric Cavity-Based Scramjet Combustor

The Implication of Injection Locations in an Axisymmetric Cavity-Based Scramjet Combustor

This paper presents the effect of cavity-based injection in an axisymmetric supersonic combustor using numerical investigation. An axisymmetric cavity-based angled and transverse injections in a circular scramjet combustor are studied. A three-dimensional Reynolds-averaged Navier–Stokes (RANS) equat...

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Bibliographic Details
Main Authors: Naresh Relangi, Antonella Ingenito, Suppandipillai Jeyakumar
Format: Article
Language:English
Published: MDPI AG 2021-05-01
Series:Energies
Subjects:
scramjet engine
axisymmetric cavity
transverse injection
computational fluid dynamics
combustion efficiency
total pressure loss
Online Access:https://www.mdpi.com/1996-1073/14/9/2626

Internet

https://www.mdpi.com/1996-1073/14/9/2626

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