Aerodynamic characteristics at subsonic and supersonic Mach numbers of a thin triangular wing of aspect ratio 2 I : maximum thickness at 20 percent of the chord
| Author: | Berggren, Robert E |
|---|---|
| Year: | 1948 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A8I16 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57967/ |