The aerodynamic characteristics of a supersonic aircraft configuration with a 40 degree sweptback wing through a Mach number range from 0 to 2.4 obtained from various sources
| Author: | Spearman, M. Leroy |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52A21 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59085/ |