Wind-Tunnel Investigation of Effect of Yawing on Lateral-Stability Characteristics 2: Rectangular N.A.C.A. 23012 Wing with a Circular Fuselage and a Fin
| Author: | Bamber, M. J. |
|---|---|
| Year: | 1939 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-730 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc54993/ |