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Aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model and aerodynamic loads on adjacent stores and missiles at Mach numbers of 1.57, 1.87, 2.16, and 2.53
| Author: | Oehman, Waldo I. |
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| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L58C17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64099/ |
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