Computational and experimental study of the influence of the shape of nozzle supersonic part on the flow structure in the gas-dynamic flow path of a model high-altitude test facility
Crossref DOI link: https://doi.org/10.1134/S0869864321020013
Published Online: 2021-07-18
Published Print: 2021-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zakharov, V. S.
Guskov, O. V.
Prokhorov, A. N.
Berezhnoy, V. N.
Text and Data Mining valid from 2021-03-01
Version of Record valid from 2021-03-01
Article History
Received: 15 July 2020
Revised: 8 December 2020
Accepted: 16 December 2020
First Online: 18 July 2021