The effect on stability and control of a pusher propeller behind conventional tail surfaces as determined by tests of a powered model in the free-flight tunnel
| Author: | Hollingworth, Thomas A |
|---|---|
| Year: | 1943 |
| Document Type: | N/A |
| Series: | NACA Wartime Reports |
| Report Number: | NACA-WR-L-220, NACA-ACR |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61007/ |