S9104BTE
S9104BTE Airfoil by Michael Selig / CC BY 4.0
DB Name: s9104BTE
Family: Selig
Max thickness: 12.0% at x = 17.20% chord
Max camber: 14.8% at x = 49.73% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
Notes:
Variant of S9104 with a blunt trailing edge. Making the trailing edge blunt converts the airfoil to having an "integral Gurney flap" in effect.
Detailed info: https://m-selig.ae.illinois.edu/uiuc_lsat/s9104/s9104.html
Released under the CC BY 4.0 license.