Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge
| Author: | Hallissy, Joseph M., Jr. |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L58E21 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64269/ |
