Wing load distribution on a swept wing airplane in flight at Mach numbers up to 1.11, and comparison with theory
| Author: | Rolls, L. Stewart |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A52A31 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59109/ |