Aerodynamic characteristics at transonic speeds of a 69 degree delta wing with a triangular plan-form control having a skewed hinge axis and an overhang balance : transonic-bump method
| Author: | Wiley, Harleth G |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50L01 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58716/ |