A summary of the drag and longitudinal trim at low lift of the North American YF-100A airplane at Mach numbers from 0.75 to 1.77 as determined by flight tests of 0.11-scale rocket models
| Author: | Blanchard, Willard S., Jr. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SL54B01 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60267/ |