Effects of vertical fins near the nose of the fuselage on the directional and damping-in-yaw stability derivatives of an airplane model under steady-state and oscillatory conditions
| Author: | Queijo, M J |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3814 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56176/ |