To the Theory of Hypersonic Flow around a Thin Delta Finite-Swept Wing at a Large Attack Angle
Crossref DOI link: https://doi.org/10.1134/S0015462820070058
Published Online: 2020-11-16
Published Print: 2020-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Golubkin, V. N.
Text and Data Mining valid from 2020-09-01
Version of Record valid from 2020-09-01
Article History
Received: 20 February 2020
Revised: 12 April 2020
Accepted: 19 April 2020
First Online: 16 November 2020