Wind-tunnel tests of ailerons at various speeds 2: ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil
| Author: | Denaci, H. G. |
|---|---|
| Year: | 1943 |
| Document Type: | N/A |
| Series: | NACA Wartime Reports |
| Report Number: | NACA-WR-L-432, NACA-ACR-3F18 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61625/ |