Wind-Tunnel Investigation of the Effects of Lip Geometry on Drag and Pressure Recovery of a Normal-Shock Nose Inlet on a Body of Revolution at Mach Numbers of 1.41 and 1.81
| Author: | Robins, A. Warner |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L57K08 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64671/ |