The effect of inlet installation on the zero-lift drag of a 60 degree delta-wing-body configuration from flight tests at Mach numbers from 0.8 to 1.86
| Author: | Merlet, Charles F. |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55I09 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61586/ |