Wind Tunnel Tests of Ailerons at Various Speeds 4: Ailerons of 0.20 Airfoil Chord and True Contour With 0.35 Aileron-Chord Extreme Blunt-Nose Balance on the NACA 23012 Airfoil
| Author: | Anderson, R. A. |
|---|---|
| Year: | 1943 |
| Document Type: | N/A |
| Series: | NACA Wartime Reports |
| Report Number: | NACA-WR-L-433, NACA-ACR-3H28 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61629/ |