Comprehensive analysis of tubular combustion chambers in Turbo-Ramjet engines for enhanced hypersonic propulsion

Comprehensive analysis of tubular combustion chambers in Turbo-Ramjet engines for enhanced hypersonic propulsion

Anticipating a doubling in global air travel demand by 2040, the present work underscores the need for innovation in aviation propulsion systems. This study presents the design and analysis of tubular combustors for lower Mach numbers in Turbo-Ramjet engines, utilizing input parameters derived from...

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Bibliographic Details
Main Authors: Nikhil S Prakash, Akhil G, Amjith L R
Format: Article
Language:English
Published: KeAi Communications Co. Ltd. 2025-06-01
Series:FirePhysChem
Subjects:
Turbo-Ramjet
Combustion
Tubular chamber
CFD
Flow analysis
Gas turbine
Online Access:http://www.sciencedirect.com/science/article/pii/S2667134424000828
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