Langley full-scale-tunnel investigation of the fuselage boundary layer on a typical fighter airplane with a single liquid-cooled engine
| Author: | Czarnecki, K. R. |
|---|---|
| Year: | 1946 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-1087 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc54857/ |