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 Luesutthiviboon *, Tercio Lima Pereira*, Daniele Ragni , Francesco Avallone , Alexandre Suryadi†, Michaela Herr†, Andreas Fischer‡

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 the option to plot the camber around the circumference of a circle and adjust the plotting grid.

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. Then, a third digit indicates the design lift coefficient.

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...