Performance analysis of a planar shaped strut injector based supersonic combustion chamber
Author:
Affiliation:
1. Mechanical Engineering Department , Visvesvaraya National Institute of Technology , Nagpur 440010 , MH , India
Abstract
Publisher
Walter de Gruyter GmbH
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2024-0024/pdf
Reference38 articles.
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2. Kummitha, OR, Pandey, KM, Gupta, R . Numerical analysis of hydrogen fueled scramjet combustor with innovative designs of strut injector. Int J Hydrogen Energy 2020;45:13659–71. https://doi.org/10.1016/j.ijhydene.2018.04.067.
3. Peng, J, Cao, Z, Yu, X, Yang, S, Yu, Y, Ren, H, et al. . Analysis of combustion instability of hydrogen fueled scramjet combustor on high-speed OH-PLIF measurements and dynamic mode decomposition. Int J Hydrogen Energy 2020;45:13108–18. https://doi.org/10.1016/j.ijhydene.2020.02.216.
4. Macleod, C, Gerrard, CE . A review of air-fuel mixing and alternative methods in scramjets and scramjet-like engines. J Br Interplanet Soc 2016;69:116–26.
5. Gugulothu, SK . A systematic literature review based on different fuel injection strategies used in scramjet combustors. Heat Transfer-Asian Res 2019;20:1–22. https://doi.org/10.1002/htj.21561.
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