Computational investigation of vortex structure and breakdown over a delta wing at supersonic pitching maneuver
Crossref DOI link: https://doi.org/10.1007/s40430-018-1021-z
Published Online: 2018-01-24
Published Print: 2018-02
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Hadidoolabi, M.
Ansarian, H. http://orcid.org/0000-0001-9685-5262
Text and Data Mining valid from 2018-01-24
Article History
Received: 10 September 2015
Accepted: 9 January 2018
First Online: 24 January 2018