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Numerical Study of Viscous Flows in Rocket Engine Nozzles with an Optimized Supersonic Part and Separation of the Laminar Boundary Layer from the Wall

Crossref DOI link: https://doi.org/10.3103/S1068799822040213

Published Online: 2023-04-26

Published Print: 2022-10

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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