Some effects of aeroelasticity and sweepback on the rolling effectiveness and drag of a 1/11-scale model of the Bell X-5 airplane wing at Mach numbers from 0.6 to 1.5
| Author: | English, Roland D |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53I18b |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc54679/ |