An analysis of surface pressures and aerodynamic load distribution over the swept wing of the Douglas D-558-II research airplane at Mach numbers from 0.73 to 1.73
| Author: | Taillon, Norman V |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-H58A30 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64095/ |