Analysis of various NACA airfoil and fabrication of wind tunnel to test the scaled-down model of an airfoil

Autor:	M Krishna, A Joshua, V. Thanigaivelan, J. Silkson John
Rok vydání:	2021
Předmět:	Airfoil Lift (force) Lift coefficient Materials science Angle of attack Drag Mechanical engineering Aerodynamics Wind tunnel NACA airfoil
Zdroj:	IOP Conference Series: Materials Science and Engineering. 1130:012021
ISSN:	1757-899X 1757-8981
DOI:	10.1088/1757-899x/1130/1/012021
Popis:	Airfoil design is a major facet of aerodynamics. Various airfoils serve different flight regimes. Asymmetric aero foils can generate lift at zero angle of attack, while a symmetric aero foils exhibit no lift at the same case. The design of the Airfoil has a great influence in the lift provided to an aircraft and the thrust required to make the lift take place. The geometry design of the airfoil is carried through Design Modeler. The analysis work of the airfoil is carried using Ansys Fluent. The coefficient of lift and drag are calculated through constant density throughout the section.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::cd3b6315da2379d0a870cea2a1611531 https://doi.org/10.1088/1757-899x/1130/1/012021 Zobrazit plný text záznamu