 |
|
Theoretical investigation of the effects of configuration changes on the center of pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transonic and supersonic speeds
| Author: | Spahr, J Richard |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A55F02 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61384/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010