Effects of SJA boundary conditions on predicting the aerodynamic behavior of NACA 0015 airfoil in separated condition
Crossref DOI link: https://doi.org/10.1007/s12206-015-0403-8
Published Online: 2015-05-16
Published Print: 2015-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Moshfeghi, Mohammad
Hur, Nahmkeon
Text and Data Mining valid from 2015-05-01