학술논문

Experimental analysis of a NACA 0021 airfoil section through 180-deg angle of attack at low Reynolds numbers for use in wind turbine analysis
Document Type
Article
Source
In: Journal of Engineering for Gas Turbines and Power. (Journal of Engineering for Gas Turbines and Power, 1 April 2019, 141(4))
Subject
Language
English
ISSN
15288919
07424795