Investigation at zero forward speed of a leading-edge slat as a longitudinal control device for vertically rising airplanes that utilize the redirected-slipstream principle
| Author: | Kuhn, Richard E |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3692 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55950/ |