Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel : influence of trailing-edge flap span and deflection on the longitudinal characteristics
| Author: | Cancro, Patrick A. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SL54H27 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60848/ |