Differences

This shows you the differences between two versions of the page.

--- searchwing-flugzeug [2019/10/06 10:59]
beckmanf airfoil
+++ searchwing-flugzeug [2019/10/06 12:44]
beckmanf pitch
@@ Line 21: / Line 21: @@
 ==== X-UAV Mini Talon ====
-The airfoil of the X-UAV Mini Talon is a [[http://airfoiltools.com/airfoil/details?airfoil=s3010-il|S3010]] with 270mm chord length. This airfoil is similar to the S3021 and the Clark-Y. The airfoil is optimised for low Reynold numbers, i.e. small wings and low speeds. The wing of the Mini Talon has a length of approx. 270mm at the fuselage. The Reynolds number is approx. R = v * l * 70 when v is the speed in m/s and l is the length in mm. At a speed of 8m/s this translates to a Reynolds number of approx. 150000.
+The airfoil of the X-UAV Mini Talon is a [[http://airfoiltools.com/airfoil/details?airfoil=s3010-il|S3010]] with 270mm chord length. The pitch is approximately 3°. This airfoil is similar to the S3021 and the Clark-Y. The airfoil is optimised for low Reynold numbers, i.e. small wings and low speeds. The wing of the Mini Talon has a length of approx. 270mm at the fuselage. The Reynolds number is approx. R = v * l * 70 when v is the speed in m/s and l is the length in mm. At a speed of 8m/s this translates to a Reynolds number of approx. 150000.
 [[https://www.aerodesign.de/profile/profile_n.htm|Aerodesign Profilkatalog]]