A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70
| Author: | Falanga, Ralph A. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55L21 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62247/ |