Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel
| Author: | Bird, John D. |
|---|---|
| Additional Authors: | Jaquet, Byron M. |
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2483 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55717/ |