Combustion dynamics of ten-injector rocket engine using flamelet progress variable

Author:

Zhan LeiORCID,Nguyen Tuan M.ORCID,Xiong Juntao,Liu FengORCID,Sirignano William A.

Funder

Stanford University

Air Force Office of Scientific Research

Publisher

Elsevier BV

Reference55 articles.

1. High-frequency combustion instability in rocket motors with concentrated combustion;Crocco;J. Am. Rocket Soc.,1953

2. High-frequency combustion instability in rockets with distributted combustion;Crocco;Symp. (Int.) Combust.,1953

3. Theory of combustion instability in liquid propellant rocket motors;Crocco,1956

4. S. Gröning, D. Suslov, M. Oschwald, T. Sattelmayer, Stability behaviour of a cylindrical rocket engine combustion chamber operated with liquid hydrogen and liquid oxygen, in: 5th European Conference for Aerospace Sciences, 2013.

5. S. Gröning, D. Suslov, J. Hardi, M. Oschwald, Influence of hydrogen temperature on the acoustics of a rocket engine combustion chamber operated with LOX/H2 at representative conditions, in: Proceedings of Space Propulsion, 2014.

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