Numerical Study of the Turbulent Boundary Layer with an Adverse Pressure Gradient in Compressible Gas Flow
Crossref DOI link: https://doi.org/10.1134/S0015462824604583
Published Online: 2025-05-08
Published Print: 2025-02
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Lushchik, V. G.
Popovich, S. S.
Text and Data Mining valid from 2025-02-01
Version of Record valid from 2025-02-01
Article History
Received: 26 September 2024
Revised: 11 October 2024
Accepted: 11 October 2024
First Online: 8 May 2025
CONFLICT OF INTEREST
: The authors of this work declare that they have no conflicts of interest.