 |
|
Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel V : static longitudinal stability and control throughout the subsonic speed range of a semispan model of a supersonic airplane
| Author: | Johnson, Ben H , Jr |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A9I01 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58320/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010