Aerodynamic Characteristics at Mach Numbers From 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight
| Author: | Carmel, Melvin M. |
|---|---|
| Additional Authors: | Kelly, Thomas C. |
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L58G16 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64406/ |