Airfoil design optimization based on lattice Boltzmann method and adjoint approach
Crossref DOI link: https://doi.org/10.1007/s10483-018-2333-9
Published Online: 2018-03-16
Published Print: 2018-06
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Li, Xiaowei
Fang, Liang
Peng, Yan
Text and Data Mining valid from 2018-03-16
Article History
Received: 18 September 2017
Revised: 23 November 2017
First Online: 16 March 2018