Lateral-control investigation of flap-type controls on a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic bump method
| Author: | Vogler, Raymond D |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50A17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58445/ |