Effect of wall cavity with combined fuel injection technique in scramjet combustor with CFD-Reference-Cited by-同舟云学术

Effect of wall cavity with combined fuel injection technique in scramjet combustor with CFD

Published:2021 Issue: Volume:45 Page:6609-6614
ISSN:2214-7853
Container-title:Materials Today: Proceedings
language:en
Short-container-title:Materials Today: Proceedings

Author:

Ambe Verma Kumari,Murari Pandey Krishna,Kumar Sharma Kaushal

Publisher

Elsevier BV

Subject

General Medicine

Reference35 articles.

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4. Q. Liu, D. Baccarella, G. Lee, T. Lee. 2019, January. Influences of Cavity on Combustion Stabilization in an Axisymmetric Scramjet. In AIAA Scitech 2019 Forum (p. 1681).

5. Computational investigation on design of scramjet combustor – A review;Verma;Int. J. Recent Technol. Eng.,2019

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1. Effect of variation of temperature on the internal flow characteristics of a strut and cavity-based SCRAMJET combustor;Interactions;2024-07-15

2. Impact of passive fuel injections techniques in the flow field of the scramjet combustor;International Journal of Thermofluids;2022-11

3. Computational investigation to interpret the reacting flow conditions for two different fuels in the scramjet combustor;Results in Engineering;2022-09

4. The numerical investigation of combustion performance of scramjet combustor with variation in angle of attack;Results in Engineering;2022-09

5. COMPUTATIONAL INVESTIGATION OF TRANSVERSE FUEL-INJECTION SCRAMJET COMBUSTOR FOR DIFFERENT INCOMING MACH NUMBERS;International Journal of Fluid Mechanics Research;2022