Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model-Reference-Cited by-同舟云学术

Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model

Published:2024-05-23 Issue: Volume: Page:
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Pallela Arvind,Kumar Shivam,Thakur Amit Kumar^ORCID,Gupta Lovi Raj,Singh Rajesh

Publisher

Springer Science and Business Media LLC

Link

https://link.springer.com/content/pdf/10.1007/s42405-024-00746-0.pdf

Reference33 articles.

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3. Li J, Fan W, Qiu H, Yan C, Wang Y-Q (2010) Preliminary study of a pulse normal detonation wave engine. Aerosp Sci Technol 14(3):161–167. https://doi.org/10.1016/j.ast.2009.12.002

4. Liu L, Zhang Q (2019) Numerical study of cellular structure in detonation of a stoichiometric mixture of vapor JP-10 in air using a quasi-detailed chemical kinetic model. Aerosp Sci Technol 91:669–678. https://doi.org/10.1016/j.ast.2019.07.017

5. Wolaski P (2011) Detonation engines. J KONES Powertrain Transp Vol. 18, No. 3, 2011. Retrieved 6 February 2023. http://arc.uta.edu/research/pde.htm. Accessed 6 Feb 2023

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1. Correction: Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model;International Journal of Aeronautical and Space Sciences;2024-06-07