Investigation of a triangular wing in conjunction with a fuselage and horizontal tail to determine downwash and longitudinal-stability characteristics: transonic bump method
| Author: | Allen, Edwin C. |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A51F12a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59054/ |