Special bodies added on a wing to reduce shock induced boundary-layer separation at high subsonic speeds
| Author: | Whitcomb, Richard T |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-4293 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57196/ |