Drag and longitudinal trim characteristics of a low-tail version of the North American YF-100A airplane as determined from the flight test at low lift of a 0.11-scale rocket-powered model at Mach numbers between 0.75 and 1.78
| Author: | Blanchard, Willard S., Jr. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SL54D05 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60785/ |