View in EDS HTML Full Text PDF Full Text

Stabilization of crossflow mode by grooves on a supersonic swept wing.

Saved in:
Bibliographic Details
Title: Stabilization of crossflow mode by grooves on a supersonic swept wing.
Authors: Fedorov, Alexander1, afedorov55@gmail.com, Novikov, Andrey1,2
Source: Theoretical & Computational Fluid Dynamics; Apr2023, Vol. 37 Issue 2, p261-268, 8p
Database: Applied Science & Technology Source
Full text is not displayed to guests.
Description
ISSN:09354964
DOI:10.1007/s00162-023-00658-x