 |
|
Experimental investigation at high subsonic speed of the rolling stability derivatives of a complete model having a clipped-delta wing and a high horizontal tail
| Author: | Sleeman, William C , Jr |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55K11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61826/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010