An investigation at Mach numbers of 1.41 and 2.01 of the aerodynamic characteristics of a swept-wing supersonic bomber configuration
| Author: | Smith, Norman F |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52J17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59555/ |