Max thickness 18% at 34.7% chord.

Max thickness 18% at 33.9% chord.

Aeroacoustic characterization of a NACA 63(3)-018 airfoil with trailing-edge serrations: a benchmarking study across facilities over a wide Reynolds number range 5 August 2021 Salil …

Aug 16, 2013 · High-speed Aerodynamic Characteristics of Four Thin NACA 63-series Airfoils. Document ID. 19930085755

Airfoil (aerofoil) plotter (NACA 63(3)-018) which allows the airfoil to be displayed and printed, from existing dat files or the user's coordinates, to the required chord width and thickness. There is …

Jul 24, 2008 · Date/Time Thumbnail Dimensions User Comment; current: 19:03, 24 July 2008: 1,600 × 1,200 (46 KB): ILA-boy (talk | contribs) == Beschreibung == {{Information ...

Performance data on the three sub-families of NACA airfoils are collected here: NACA 63, NACA 64 and NACA 65. They differ from each other by the chordwise position of minimum pressure. …

Aug 26, 2012 · Dear Friends, NACA 6311. and NACA 6318 Is these airfoils are low Re number aerofoils?

After analysis among five airfoils three airfoils were chosen (NACA: 6318, 9520, 9525) which having higher Cd and lower Cl values.

Download scientific diagram | Lift and drag coefficients on NACA 63-618 at different discharge frequencies at 20 m/s and α = 15 deg. from publication: Experimental Study and Numerical...