Improved vortex lattice method for drag prediction of supersonic wings using shock cone modelling
Crossref DOI link: https://doi.org/10.1007/s00366-025-02192-2
Published Online: 2025-08-13
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Joshi, Hemant
Thomas, Peter
Tan, Christabel
Wu, Hongwei
Text and Data Mining valid from 2025-08-13
Version of Record valid from 2025-08-13
Article History
Received: 8 November 2024
Accepted: 30 July 2025
First Online: 13 August 2025
Declarations
:
: The authors declare no Conflict of interest.