Experimental Investigation of High-Angle-of-Attack Aerodynamics of Low-Aspect-Ratio Rectangular Wings Configured with NACA0012 Airfoil Section
Crossref DOI link: https://doi.org/10.1007/s42405-019-00215-z
Published Online: 2019-09-13
Published Print: 2020-06
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Lee, Seok Ho
Han, Yong Oun http://orcid.org/0000-0001-9625-9049
Text and Data Mining valid from 2019-09-13
Version of Record valid from 2019-09-13
Article History
Received: 5 April 2019
Revised: 1 September 2019
Accepted: 5 September 2019
First Online: 13 September 2019