Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen
Crossref DOI link: https://doi.org/10.1007/s12567-016-0130-8
Published Online: 2016-07-09
Published Print: 2017-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Gröning, Stefan
Hardi, Justin
Suslov, Dmitry
Oschwald, Michael
Funding for this research was provided by:
Deutsche Forschungsgemeinschaft (SFB TR40)
License valid from 2016-07-09