Wind Tunnel Tests of Ailerons at Various Speeds 1: Ailerons of 0.20 Airfoil Chord and True Contour With 0.35 Aileron-Chord Extreme Blunt Nose Balance on the NACA 66,2-216 Airfoil
| Author: | Letko, W. |
|---|---|
| Additional Authors: | Denaci, H. G. |
| Year: | 1943 |
| Document Type: | N/A |
| Series: | NACA Wartime Reports |
| Report Number: | NACA-WR-L-431, NACA-ACR-3F11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61624/ |