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eNauka >  Results >  Two-component propellant grain for rocket motor combustion analysis and geometric optimization
Title: Two-component propellant grain for rocket motor combustion analysis and geometric optimization
Authors: Alazeezi, Mohammed; Popović, Nikola P.; Elek, Predrag  
Issue Date: 2022
Publication: Thermal Science
ISSN: 0354-9836 Thermal Science Search Idenfier
Publisher: Univerzitet u Beogradu - Institut za nuklearne nauke Vinča, Beograd
Type: Article
Collation: vol. 26 br. 2 str. 1567-1578
DOI: 10.2298/TSCI210604290A
WoS-ID: 000791221600026
Scopus-ID: 2-s2.0-85126919544
URI: https://enauka.gov.rs/handle/123456789/573717
https://machinery.mas.bg.ac.rs/handle/123456789/3788
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