Improved vortex lattice method for drag prediction of supersonic wings using shock cone modelling

  1. Hemant Joshi
  2. Peter Thomas
  3. Christabel Tan
  4. Hongwei Wu
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  1. Version published to 10.1007/s00366-025-02192-2
  2. Version published to 10.21203/rs.3.rs-5418595/v1 on Research Square