Assessment of thrust chamber stability margins to high-frequency oscillations based on mathematical modeling of coupled ‘injector–rocket combustion chamber’ dynamic system / Nikolayev O. D., Bashliy I. D. (2022)
UkrainianEnglish

web address of the page http://jnas.nbuv.gov.ua/article/UJRN-0001604442
  Technical mechanics   Б - 2020  /     Issue (2022, № 1)

Nikolayev O. D., Bashliy I. D.
Assessment of thrust chamber stability margins to high-frequency oscillations based on mathematical modeling of coupled ‘injector–rocket combustion chamber’ dynamic system

Бібліографічний опис:
Nikolayev O. D., Bashliy I. D. Assessment of thrust chamber stability margins to high-frequency oscillations based on mathematical modeling of coupled ‘injector–rocket combustion chamber’ dynamic system. Технічна механіка. 2022. № 1. С. 3-15. URL: http://jnas.nbuv.gov.ua/article/UJRN-0001604442

 

Institute of Information Technologies of VNLU

+38 (044) 525-36-24
libnas@nbuv.gov.ua
Ukraine, 03039, Kyiv, Holosiivskyi Ave, 3, room 209