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Effects of Leading Edge Radius on Stall Characteristics of Rotor Airfoil

The effects of leading edge radius on the static and dynamic stall characteristics of rotor airfoils are investigated. Initially, a parametric airfoil (PARFOIL) method is employed to generate four morphed airfoils with different leading edge radii based on a NACA 0012 airfoil. Subsequently, the Reyn...

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Gorde:
Xehetasun bibliografikoak
Egile Nagusiak: Simeng Jing, Guoqing Zhao, Yuan Gao, Qijun Zhao
Formatua: Artigo
Hizkuntza:Inglês
Argitaratua: MDPI AG 2024-06-01
Saila:Aerospace
Gaiak:
Sarrera elektronikoa:https://www.mdpi.com/2226-4310/11/6/470
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