Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen

Author:

Gröning Stefan,Hardi Justin,Suslov Dmitry,Oschwald Michael

Funder

Deutsche Forschungsgemeinschaft

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference60 articles.

1. Anderson, W.E., Ryan, H.M., Santoro, R.J.: Combustion instability phenomena of importance to liquid bi-propellant rocket engine. In: 28th JANNAF Combustion Subcommittee Meeting (1991)

2. Barrère, M., Williams, F.A.: Comparison of combustion instabilities found in various types of combustion chambers. In: Symposium (International) on Combustion, vol. 12, pp. 169–181. The Combustion Institute, Pittsburgh (1969). doi: 10.1016/S0082-0784(69)80401-7

3. Bendat, J.S., Piersol, A.G.: Engineering Applications of Correlation and Spectral Analysis. Wiley, New York (1993)

4. Bilstein, R.E.: Stages to saturn. NASA Special Publication, National Aeronautics and Space Administration, Washington DC (1980). NASA SP-4206

5. Candel, S.: Combustion dynamics and control: progress and challenges. In: Proceedings of the Combustion Institute, vol. 29, pp. 1–28. The Combustion Institute (2002). doi: 10.1016/S1540-7489(02)80007-4

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