 |
|
An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback: Static longitudinal stability and control characteristics at a Mach number of 1.59
| Author: | Spearman, M. Leroy |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50E12 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58494/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010