The Effect of Sweepback on the Longitudinal Characteristics at a Mach Number of 1.24 of a 1/30 Scale Semispan Model of the Bell X-5 Airplane From Tests by the NACA Wing Flow Method
| Author: | Morris, Garland J. |
|---|---|
| Additional Authors: | Kennedy, Robert M. |
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50I28 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58683/ |