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 speeds
| Author: | Spahr, J Richard |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3966 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56462/ |