3D versus 2D calculation of thrust characteristics of the air-breathing pulse detonation engine under supersonic flight conditions
Crossref DOI link: https://doi.org/10.1134/S1990793114110244
Published Online: 2015-01-28
Published Print: 2014-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zangiev, A. E.
Ivanov, V. S.
Frolov, S. M.
Text and Data Mining valid from 2014-11-01