Flight determination of the drag of conical-shock nose inlets with various cowling shapes and axial positions of the center body at Mach numbers from 0.8 to 2.0
| Author: | Merlet, Charles F. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54G21a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60771/ |