 |
|
Rolling Effectiveness of a Thin Tapered Wing Having Partial-Span Ailerons as Determined by Rocket-Powered Test Vehicles
| Author: | Sandahl, Carl A. |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50D17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58538/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010