Free-flight investigation to obtain drag-at-lift and stability data for a 60 degree delta-wing-body configuration over a Mach number range of 1.3 to 1.6
| Author: | Welsh, Clement J |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55G14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61582/ |