Investigation and Comparison of Stall Angle of Airfoil NACA 0012 in Reynolds Number of 3 × 106 with K‑ω SST, Realizable k‑ε, Spalart-Allmaras Turbulence Models

Autor:	Mohammad Bigdeli, Vahid Monfared
Rok vydání:	2020
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::9a1b2a527364ea8ee0b945f89406ea84 https://doi.org/10.7546/crabs.2020.03.13 Zobrazit plný text záznamu