Effect of wing flexibility on the damping roll of a notched delta-wing body combination between Mach numbers 0.6 and approximately 2.2 as determined with rocket-propelled models
| Author: | Bland, William M , Jr |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54E04 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60607/ |