Experimental investigation of the effect of vertical-tail size and length of fuselage shape and length on the static lateral stability characteristics of a model with 45 degree sweptback wing and tail surfaces
| Author: | Queijo, M J |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2168 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55722/ |