Effect of Different Shock Generator Configurations on Ethylene-Fuelled Transverse Injection-Based Scramjet Combustor

Author:

Yadav Pabbala Monish,Choubey Gautam,Tripathi Sumit

Publisher

Springer Nature Singapore

Reference36 articles.

1. Curran, E.T., Murthy, S.N.B. (eds.): Scramjet propulsion, 1st edn. American Institute of Aeronautics and Astronautics, Reston (2001)

2. Segal, C.: The Scramjet Engine: Processes and Characteristics, 1st edn. Cambridge University Press, Cambridge (2009)

3. Hyungseok, S.: A study of the mixing characteristics for cavity sizes in scramjet engine combustor. J. Korean Phys. Soc. 55(5), 2180–2186 (2009)

4. Huang, W., et al.: Investigation on the flameholding mechanisms in supersonic flows: backward-facing step and cavity flameholder. J. Visualization 14(1), 63–74 (2011)

5. Bogdanoff, D.W.: Advanced injection and mixing techniques for scramjet combustors. J. Propul. Power 10(2), 183–190 (1994)

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