The effects of sweepback on longitudinal characteristics of a 1/30-scale semispan model of the Bell X-5 airplane as determined from NACA wing-flow tests at transonic speeds
| Author: | Kolnick, Joseph J. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52I23 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59388/ |