Estimation of aerodynamic coefficients of a non-slender delta wing under ground effect using artificial intelligence techniques
Crossref DOI link: https://doi.org/10.1007/s00521-022-07013-x
Published Online: 2022-02-21
Published Print: 2022-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Tumse, Sergen
Bilgili, Mehmet
Sahin, Besir https://orcid.org/0000-0003-0671-0890
Text and Data Mining valid from 2022-02-21
Version of Record valid from 2022-02-21
Article History
Received: 7 July 2021
Accepted: 30 January 2022
First Online: 21 February 2022
Declarations
:
: The authors declare that they have no conflict of interest.