Some Effects of Spanwise Aileron Location and Wing Structural Rigidity on the Rolling Effectiveness of 0.3-Chord Flap-Type Ailerons on a Tapered Wing Having 63 Degrees Sweepback at the Leading Edge and Naca 64A005 Airfoil Sections
| Author: | Strass, H. Kurt |
|---|---|
| Additional Authors: | Fields, E. M. |
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51D18a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58986/ |