Highly resolved numerical simulation of combustion downstream of a rocket engine igniter
Crossref DOI link: https://doi.org/10.1007/s00193-017-0715-y
Published Online: 2017-02-28
Published Print: 2017-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Buttay, R.
Gomet, L.
Lehnasch, G.
Mura, A.
License valid from 2017-02-28