Investigation of the downwash and wake behind a triangular wing of aspect ratio 4 at subsonic and supersonic Mach numbers
| Author: | Walker, Harold J |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A50I14a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58680/ |