Determination of the Flow Field in the Propellant Tank of a Rocket Engine on Completion of the Mission
Crossref DOI link: https://doi.org/10.1007/s10891-018-1752-9
Published Online: 2018-05-05
Published Print: 2018-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Fedorov, A. V.
Bedarev, I. A.
Lavruk, S. A.
Trushlyakov, V. I.
Kudentsov, V. Yu.
Text and Data Mining valid from 2018-03-01
Article History
Received: 16 June 2016
First Online: 5 May 2018