Computational investigation to interpret the reacting flow conditions for two different fuels in the scramjet combustor

The scramjet engines use the atmospheric oxygen to complete the combustion process, therefore, known as Air breathing engines. It does not bear any active parts and operates at supersonic speed, so it becomes essential that the variables such as fuel, pressure, temperature, Mach number to create the...

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Bibliographic Details
Main Authors: Namrata Bordoloi, Krishna Murari Pandey, Mukul Ray, Kaushal Kumar Sharma
Format: Article
Language:English
Published: Elsevier 2022-09-01
Series:Results in Engineering
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2590123022002389