Preliminary drag measurements of the consolidated Vultee XF-92A delta-wing airplane in flight tests to a Mach number of 1.01
| Author: | Bellman, Donald R. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53J23 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59900/ |