Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations
| Author: | Dryer, Murray |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E57K26 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64014/ |