Optimization of a subsonic wind tunnel nozzle with low contraction ratio via ball-spine inverse design method
Crossref DOI link: https://doi.org/10.1007/s12206-016-0412-2
Published Online: 2016-05-27
Published Print: 2016-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Hoghooghi, Hadi
Ahmadabadi, Mahdi Nili
Manshadi, Mojtaba Dehghan
Text and Data Mining valid from 2016-05-01