Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9 1 - Wing Tip With Subsonic Leading Edge
| Author: | Jagger, James M. |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E8K26 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57955/ |