Computational investigation of mixing performance on the effects of innovative transverse fuel injection system in parallel fuel injection based scramjet combustor-Reference-Cited by-同舟云学术

Computational investigation of mixing performance on the effects of innovative transverse fuel injection system in parallel fuel injection based scramjet combustor

Published:2021 Issue: Volume:38 Page:2452-2456
ISSN:2214-7853
Container-title:Materials Today: Proceedings
language:en
Short-container-title:Materials Today: Proceedings

Author:

Verma Kumari Ambe,Pandey Krishna Murari,Sharma Kaushal Kumar

Publisher

Elsevier BV

Subject

General Medicine

Reference14 articles.

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

3. Numerical study of combustion effects on the development of supersonic turbulent mixing layer flows with WENO schemes;Liu;Comp. Fluids,2019

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

5. Dynamics and mixing mechanism of transverse jet injection into a supersonic combustor with cavity flameholder;Liu;Acta Astronautica.,2017

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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. CFD-Based Numerical Analysis of a Scramjet Combustor with the Dual Cavity for Inlet Mach Number at 7 with Hydrogen as a Fuel;Lecture Notes in Mechanical Engineering;2024

3. A Review of the Current Challenges on the Issues of Scramjet Combustion Engines;Materials and Technologies for a Green Environment;2023-03-21

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

5. Impact of Wall Fuel and Air Injections Inside the Parallel Fuel Injection-Based Scramjet Combustor: A Numerical Analysis;Lecture Notes in Mechanical Engineering;2022-09-21