Unsteady streamlines near the trailing edge of naca 0012 airfoil at a reynolds number of 125,000

Liu, X.L.X.L.LiuWo, A.A.WoCovert, E.E.E.E.CovertANDREW WO2020-04-282020-04-281990https://scholars.lib.ntu.edu.tw/handle/123456789/485896[SDGs]SDG13Unsteady streamlines near the trailing edge of naca 0012 airfoil at a reynolds number of 125,000journal article10.2514/3.103682-s2.0-0025263053https://www.scopus.com/inward/record.uri?eid=2-s2.0-0025263053&doi=10.2514%2f3.10368&partnerID=40&md5=d7b48d46a8135f704b2b2e0e1dee122b