Aerodynamic characteristics at Mach numbers from 0.7 to 1.75 of a four-engine swept-wing airplane configuration as obtained from a rocket-propelled model test
| Author: | Chapman, Rowe, Jr. |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55F23 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62214/ |