Effect of unit Reynolds number on the laminar-turbulent transition on a swept wing in supersonic flow
Crossref DOI link: https://doi.org/10.1134/S0869864318050025
Published Online: 2018-12-26
Published Print: 2018-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Ermolaev, Yu. G.
Kosinov, A. D.
Semenov, A. N.
Semionov, N. V.
Yatskikh, A. A.
Text and Data Mining valid from 2018-09-01
Article History
Received: 12 April 2018
Revised: 17 May 2018
First Online: 26 December 2018