9. Modeling of Cyclone-4M Rocket Jet Acoustic Emission by Volumetric Source
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine1; Oles Honchar Dnipro National University, Dnipro, Ukraine2
Page: Kosm. teh. Raket. vooruž. 2019, (1); 64-71
DOI: https://doi.org/10.33136/stma2019.01.064
Language: Russian
Key words: integrated launch vehicle, acoustic field, sound pressure
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