Details: Dat file: Parser (usa35b-il) USA-35B AIRFOIL USA-35B airfoil Max thickness 11.6% at 30% chord. Max camber 4.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file

Airfoil (aerofoil) plot of USA-35B AIRFOIL with ajustable chord width, camber and thickness and full size print out

2009年9月27日 · I've flown the NACA 23012 on the Tcrafts, the USA-35B mod on the Cubs (clipped and full-span), and the NACA 4412 on Champs. They all flew a little different, but none were dangerous if you knew what to expect.

usa-35b airfoil 17.0 17.0 0.0000000 0.0000000 0.0125000 0.0239000 0.0250000 0.0335000 0.0500000 0.0476000 0.0750000 0.0589000 0.1000000 0.0669000 0.1500000 0.0780000 0.2000000 0.0852000 0.3000000 0.0900000 0.4000000 0.0866000 0.5000000 0.0757000 0.6000000 0.0605000 0.7000000 0.0432000 0.8000000 0.0226000 0.9000000 -.0004000 0.9500000 -.0126000 1.0000000 -.0251000 0.0000000 0.0000000 0.0125000 ...

2013年1月7日 · A pair of longitudinal ridges is employed to enhance the aerodynamic efficiency of an USA-35B airfoil used in a remotely controlled aircraft wing. Measurements include surface static pressure...

Polar details for airfoil (aerofoil)USA-35B AIRFOIL(usa35b-il) Xfoil prediction at Reynolds number 1,000,000 and Ncrit 9

2003年1月4日 · I have been reading with great interest the discussions regarding the modifications to the Cub wing to make it perform better in the landing and take-off modes of operation. When the Cub was designed in the 1930's, and the U.S.A. 35B was chosen to be the airfoil for the Cub, it turned out to be a very good choice, and has stood the test of time.

2022年6月16日 · Hello everyone, I need of experimental data from USA 35B airfoil, is to an academic work (homework). Where can I find experimental data from this airfoil? I tried airfoiltools.com (I find the airfoil I want, but not experimental data) and others coordinates sites.

USA 35B - Free download as PDF File (.pdf), Text File (.txt) or read online for free. This document describes an airfoil named USA-35B with a chord of 100mm, radius of 0mm, thickness of 100% of the chord, and an origin and pitch of 0 degrees.

2014年7月27日 · USA 35B Airfoil Analysis. Coefficient Data. Reference: http://www.worldofkrauss.com/foils/1061. Slideshow 2440120 by euclid